Airplane Flight Manuals (Piper Reports and Supplements) #
WORK IN PROGRESS #
If you have scans of the following unavailable reports, please upload it to our dropbox!
Overview #
For the singles - the TCDS specifies the core AFM report (called “Section 1”), along with the supplements required based on equipment as configured. The first table presents full AFMs with all available suppliments. The second table is a direct breakdown of each report and suppliment by TCDS line.
Suppliment 1770 adds Vne restrictions.
For the twins - the TCDS is much simpler, only calling out four reports by serial number.
Airplane Flight Manuals Assembled / Summary #
Note: the linked documents below are not yet assembled into a full AFM report, as I do not have any “complete” reports with all supplements. Once all supplements for a report have been collected, a complete report will be assembled. In the interim, download and assemble as needed.
Singles #
| Report Number | Eligibility | Included Documents | TCDS §401 References |
|---|---|---|---|
| Unkn | S/N 24-2 through 24-102 only. | Supplement No. 1 | (a), (b) |
| 973 | PA-24-250, S/N 24-1, 24-103 through 24-332 | Supplement No. 1, Supplement No. 2 | (c), (e), (j) |
| Unkn | PA-24, S/N 24-103 through 24-1683 only. | Supplement No. 2 | (d), (i), note: no reference to Supplement No. 1 |
| 997 | PA-24-250, S/N 24-1, 24-103 through 24-2002, 24-2004 through 24-2298 only. Required when Item 109(a), (b), (c), or (d) is installed. | Supplement No. 1, Supplement No. 2 | (f), (g), (h) |
| 1047 | PA-24, S/N 24-1684 through 24-3687 only. Required when Item 111 is installed. | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5 | (k), (l), (m), (r), (y), (ac) |
| 1127 | PA-24-250, S/N 24-2003, 24-2299 through 24-2562, and 24-2564 through 24-2843 only with Item 112 | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5 | (n), (o), (p), (q), (z), (ad), |
| 1179 | PA-24-250, S/N 24-2563, 24-2844 through 24-3687, except when Item 109(e) is installed | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4 | (s), (t), (u), (aa), (ae), |
| 1220 | PA-24-250, S/N 24-2563, and 24-2844 through 24-3687 only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, | (v), (w), (x), (ab), (af) |
| 1295 | PA-24-400 only. | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4 | (ag), (an), (ao), (ap), (as) |
| 1333 | PA-24-260 (Carburetor Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, | (ah), (aj), (ai), (aq), (at) |
| 1334 | PA-24-260 (Fuel Injection Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5 | (ak), (al), (am), (ar), (au), (bv), |
| 1358 | PA-24-260 (Carburetor Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5, Supplement No. 6, Supplement No. 7, | (av), (aw), (ax), (ay), (az), (bf), (bh), (bj) |
| 1359 | PA-24-260 (Fuel Injection Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5, Supplement No. 6, Supplement No. 7, Supplement No. 8, | (ba), (bb), (bc), (bd), (be), (bg), (bi), (bk), (bw) |
| 1545 | PA-24-260, S/N 24-4783, and 24-4804 through 24-5034 only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5 | (bo), (bl), (bm), (bn), (bu), (bx) |
| 1640 | PA-24-260 (equipped with Turbocharger), S/N 24-4783, and 24-4804 through 24-5034 only | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5 | (bp), (bq), (br), (bs), (bt), (by) |
Twins #
| Report Number | Eligibility | Included Documents | TCDS References |
|---|---|---|---|
| 1269 | PA-30, Serial Nos. 30-1 through 30-1716 and 30-1718 through 30-1744. | Supplement No. 1, Supplement No. 2, Supplement No. 3, Supplement No. 4, Supplement No. 5, Supplement No. 6, Supplement No. 7, Supplement No. 8, Supplement No. 9, Supplement No. 10, Supplement No. 11, Supplement No. 13, AD 98-04-27 | 2. (a) and Note 5 (a) |
| 1515 | PA-30, Serial Nos. 30-1717 and 30-1745 through 3-2000 | 2. (b) and Note 5(b) | |
| 1605 | PA-39, Serial No. 39-1 through 39-162 | 2. (c) | |
| 1840 | PA-40, Serial No. 40-7400002 | 2. (d) |
Airplane Flight Manual (Singles) - TCDS Ordered by Report #
| TCDS §401 | TCDS Text | Report Number | Eligibility/Notes | |
|---|---|---|---|---|
| (a) | DMCR Approved Airplane Flight Manual dated June 19, 1957, revised March 7, 1958. Eligible for S/N 24-2 through 24-102 only. | Report ? | Eligible for S/N 24-2 through 24-102 only. | |
| (b) | DMCR Approved Airplane Supplement No. 1, revised November 11, 1958, to Airplane Flight Manual Item 401(a). Required when Item 2(a) or 6(a) is installed. | 2(a) = Propeller - McCauley constant speed controllable, hub model 2D36C14 6(a) = Deleted October 24, 1960. | ||
| (c) | DMCR Approved Airplane Flight Manual dated April 16, 1958. Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-332. | Report ? | Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-332. | |
| (e) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated May 5, 1958, to Airplane Flight Manual for Model PA-24-250, Item 401(c). Required when Item 5(a) is installed. | 5(a) = Propeller - McCauley constant speed controllable, hub model 2D36C28 | ||
| (j) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated July 31, 1958, to Airplane Flight Manual Supplement No. 973 for Model PA-24-250, Item 401(c). Required when Item 402(a), Piper AutoControl, is installed | |||
| (d) | DMCR Approved Airplane Flight Manual dated March 7, 1958. Eligible Model for PA-24, S/N 24-103 through 24-1683 only. | Report ? | Eligible Model for PA-24, S/N 24-103 through 24-1683 only. | |
| (i) | DMCR Approved Airplane Flight Manual Supplement No. 2 dated July 31, 1958, to Airplane Flight Manual for Model PA-24, Item 401(d). Required when Item 402(a), Piper AutoControl, is installed. | |||
| (f) | DMCR Approved Airplane Flight Manual No. 997 dated July 10, 1958. Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-2002, 24-2004 through 24-2298 only. Required when Item 109(a), (b), (c), or (d) is installed. | Report 997 | Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-2002, 24-2004 through 24-2298 only. Required when Item 109(a), (b), (c), or (d) is installed. 109(a) = O-540-A1A5 109(b) = O-540-A1B5 109(c) = O-540-A1C5 109(d) = O-540-A1D5 | |
| (g) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated July 10, 1958, revised August 15, 1958, to Airplane Flight Manual No. 997 for Model PA-24-250, Item 401(f). Required when Item 5(a) is installed. | 5(a) = Propeller - McCauley constant speed controllable, hub model 2D36C28 | ||
| (h) | DMCR Approved Airplane Flight Manual Supplement No. 2 dated July 31, 1958, to Airplane Flight Manual No. 997 for Model PA-24-250, Item 401(f). Required when Item 402(a), Piper AutoControl, is installed. | |||
| (k) | DMCR Approved Airplane Flight Manual No. 1047, dated December 11, 1959. Eligible for Model PA-24, S/N 24-1684 through 24-3687 only. Required when Item 111 is installed. | Report 1047 | Eligible for Model PA-24, S/N 24-1684 through 24-3687 only. Required when Item 111 is installed. 111 = Engine relocated per Piper Dwg. No. 22000. Eligible on Model PA-24, S/N 24-1684 through 24-3687; O-360-A1A or O-360-A1D | |
| (l) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated December 11, 1959, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 2(a) is installed. | 2(a) = Propeller - McCauley constant speed controllable, hub model 2D36C14 | ||
| (m) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated December 11, 1959, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(a) is installed. Revision dated June 28, 1962, required when Course Selector directional gyro is installed. | |||
| (r) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated December 13, 1960, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(b), Piper Altimatic, is installed. | |||
| (y) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 7, 1962, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (ac) | DMCR Approved Airplane Flight Manual Supplement No. 5, dated August 15, 1962, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (n) | DMCR Approved Airplane Flight Manual No. 1127, dated September 27, 1960. Eligible for Model PA-24-250, S/N 24-2003, 24-2299 through 24-2562, and 24-2564 through 24-2843 only. Required when Item 112 is installed. | Report 1127 | Eligible for Model PA-24-250, S/N 24-2003, 24-2299 through 24-2562, and 24-2564 through 24-2843 only. Required when Item 112 is installed. 112 = Two 15 gallon auxiliary wing fuel tanks. Eligible on Models PA-24-250 and PA-24-260, S/N 24-2003, 24-2299 through 24-5034. | |
| (o) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated September 27, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 5(a) is installed. | 5(a) = Propeller - McCauley constant speed controllable, hub model 2D36C28 | ||
| (p) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated September 27, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401 (n). Required when Item 402(a), Piper AutoControl, is installed. | |||
| (q) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated December 13, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(b), Piper Altimatic, is installed. | |||
| (z) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 7, 1962, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (ad) | DMCR Approved Airplane Flight Manual Supplement No. 5, dated August 15, 1962, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (s) | DMCR Approved Airplane Flight Manual No. 1179, dated September 18, 1961. Eligible for Model PA-24-250, S/N 24-2563, 24-2844 through 24-3687, except when Item 109(e) is installed. | Report 1179 | Eligible for Model PA-24-250, S/N 24-2563, 24-2844 through 24-3687, except when Item 109(e) is installed. 109(e) = IO-540-C1B5 (Fuel injection installed per Piper Dwg. No. 23144) | |
| (t) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated September 18, 1961, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(a), Piper AutoControl, is installed. Revision dated June 28, 1962, required when Course Selector directional gyro is installed. | |||
| (u) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated September 18, 1961, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(b), Piper Altimatic, is installed. | |||
| (aa) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated August 7, 1962 to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (ae) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 15, 1962, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (v) | DMCR Approved Airplane Flight Manual No. 1220, dated February 15, 1962. Eligible for Model PA-24-250, S/N 24-2563, and 24-2844 through 24-3687 only. Required when Item 109(e) is installed. | Report 1120 | Eligible for Model PA-24-250, S/N 24-2563, and 24-2844 through 24-3687 only. Required when Item 109(e) is installed. 109(e) = IO-540-C1B5 (Fuel injection installed per Piper Dwg. No. 23144) | |
| (w) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated February 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(a), Piper AutoControl, is installed with Item 109(e). Revision dated June 28, 1962, required when Course Selector directional gyro is installed. | |||
| (x) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated February 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(b), Piper Altimatic, is installed with Item 109(e). | |||
| (ab) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated August 7, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(c), Piper Altimatic II, is installed with Item 109(e). | |||
| (af) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(d), Piper AutoControl II, is installed with Item 109(e). | |||
| (ag) | DMCR Approved Airplane Flight Manual No. 1295, dated December 27, 1963. Eligible for Model PA-24-400 only. | Report 1295 | Eligible for Model PA-24-400 only. | |
| (an) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated May 5, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (ao) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated May 5, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (ap) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 607(a) is installed. | 607(a) = Exhaust Gas Temperature Indicator per STC SA788WE, installed per Piper Drawing 25287 | ||
| (as) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 609(a) is installed. | 609(a) = Oxygen System Installation per Piper Dwg. 25342. For Model PA-24-260, eligible only on S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299. | ||
| (ah) | DMCR Approved Airplane Flight Manual No. 1333, dated June 19, 1964. Eligible for Model PA-24-260 (Carburetor Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. | Report 1333 | Eligible for Model PA-24-260 (Carburetor Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. | |
| (ai) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (aj) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (aq) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 607(a) is installed. | 607(a) = Exhaust Gas Temperature Indicator per STC SA788WE, installed per Piper Drawing 25287 | ||
| (at) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401 (ah). Required when Item 609(a), Oxygen System, is installed. | 609(a) = Oxygen System Installation per Piper Dwg. 25342. For Model PA-24-260, eligible only on S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299. | ||
| (ak) | DMCR Approved Airplane Flight Manual No. 1334, dated June 19, 1964. Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. | Report 1334 | Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. | |
| (al) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (am) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 420(d), Piper Auto Control II, is installed. | |||
| (ar) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 607(a) is installed. | 607(a) = Exhaust Gas Temperature Indicator per STC SA788WE, installed per Piper Drawing 25287 | ||
| (au) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 609(a), Oxygen System, is installed. | 609(a) = Oxygen System Installation per Piper Dwg. 25342. For Model PA-24-260, eligible only on S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299. | ||
| (bv) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1334. Required when Item 123, Manually Controlled Heated Alternate Engine Induction Air, is installed. | |||
| (av) | DMCR Approved Airplane Flight Manual No. 1358, dated June 30, 1965, revised December 21, 1965, and January 6, 1966. Eligible for Model PA-24-260 (Carburetor Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. | Report 1358 | Eligible for Model PA-24-260 (Carburetor Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. | |
| (aw) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401 (av). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (ax) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (ay) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 607(a) or 607 (b), Exhaust Gas Temperature Indicator, is installed. | 607(a) = Exhaust Gas Temperature Indicator per STC SA788WE, installed per Piper Drawing 25287 607(b) = Exhaust Gas Temperature Indicator per STC SA522SW, installed per Piper Drawing 25667 | ||
| (az) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 609(b), Oxygen System, is installed. | 609(b) = Oxygen System Installation per Piper Dwg. 25542 or 25724 or 26682. For Model PA-24-260, eligible only on S/N 24-4247, and 24-4300 through 24-5034 | ||
| (bf) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5, dated May 27, 1966, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(e), Piper AutoControl II (Model AK161), is installed. | |||
| (bh) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 6, dated August 5, 1966, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(f), Piper Altimatic III, is installed. | |||
| (bj) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 7, dated August 7, 1967, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 607(c), Exhaust Gas Temperature Indicator, is installed. | |||
| (ba) | DMCR Approved Airplane Flight Manual No. 1359, dated June 30, 1965, revised December 21, 1965, and January 6, 1966. Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. | Report 1359 | Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. | |
| (bb) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(c), Piper Altimatic II, is installed. | |||
| (bc) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(d), Piper AutoControl II, is installed. | |||
| (bd) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated June 30, 1965, to Airplane Flight Manual No.1359, for Model PA-24-260, Item 401(ba). Required when Item 607(a) or 607(b), Exhaust Gas Temperature Indicator, is installed. | 607(a) = Exhaust Gas Temperature Indicator per STC SA788WE, installed per Piper Drawing 25287 607(b) = Exhaust Gas Temperature Indicator per STC SA522SW, installed per Piper Drawing 25667 | ||
| (be) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 609(b), Oxygen System, is installed. | 609(b) = Oxygen System Installation per Piper Dwg. 25542 or 25724 or 26682. For Model PA-24-260, eligible only on S/N 24-4247, and 24-4300 through 24-5034 | ||
| (bg) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5, dated May 27, 1966, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(e), Piper AutoControl III (Model AK161), is installed. | |||
| (bi) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 6, dated August 5, 1966, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(f), Piper Altimatic III, is installed. | |||
| (bk) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 7, dated August 7, 1967, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401 (ba). Required when Item 607(c), Exhaust Gas Temperature Indicator, is installed. | |||
| (bw) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 8 to Airplane Flight Manual No. 1359. Required when Item 123, Manually Controlled Heated Alternate Engine Induction Air, is installed. | |||
| (bo) | D.O.A. No. EA-1 Approved Airplane Flight Manual No. 1545, dated April 11, 1969. Eligible for Model PA-24-260, S/N 24-4783, and 24-4804 through 24-5034 only. | Report 1545 | Eligible for Model PA-24-260, S/N 24-4783, and 24-4804 through 24-5034 only. | |
| (bl) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 1 to Airplane Flight Manual No. 1545. Required when Item 402(g), AutoControl III, is installed. | |||
| (bm) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 2 to Airplane Flight Manual No. 1545. Required when Item 402(h), Altimatic IIIB, is installed. | |||
| (bn) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 3 to Airplane Flight Manual No. 1545. Required when Item 609(b), Oxygen System, is installed. | |||
| (bu) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 4 to Airplane Flight Manual No. 1545. Required when Item 304(c) or 307(a) strobe light is installed. | |||
| (bx) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1545. Required when Item 402(i), Altimatic IIIB1, is installed. | |||
| (bp) | D.O.A. No. EA-1 Approved Airplane Flight Manual No. 1640, dated May 25, 1970. Eligible Model for PA-24-260 (equipped with Turbocharger), S/N 24-4783, and 24-4804 through 24-5034 only. | Report 1640 | Eligible Model for PA-24-260 (equipped with Turbocharger), S/N 24-4783, and 24-4804 through 24-5034 only. | |
| (bq) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 1 to Airplane Flight Manual No. 1640. Required when Item 402(g), AutoControl III, is installed. | |||
| (br) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 2 to Airplane Flight Manual No. 1640. Required when Item 402(h), Altimatic IIIB, is installed. | |||
| (bs) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 3 to Airplane Flight Manual No. 1640. Required when Item 609(b), Oxygen System, is installed. | |||
| (bt) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 4 to Airplane Flight Manual No. 1640. Required when Item 304(c) or 307(a) strobe light is installed. | |||
| (by) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1640. Required when Item 402(i), Altimatic IIIB1, is installed. | |||
| (bz) | D.O.A. No. EA-1 approved Airplane Flight Manual Supplement No. 1770 for Models PA-24-250 and PA-24-260 Airplane Flight Manuals dated August 8, 1972, revised September 5 and September 27, 1972. (Copies of Supplement No. 1770 dated August 8, 1972, with no revision date are eligible and approved for use. Copies with two revision dates (September 5 and September 27, 1972) are eligible and approved for use. Copies with only one revision date (September 5, 1972) are not eligible for use.) | Supplement 1770 | Req’d by 617. (a) Balance Weight - Rudder. Install in accordance with Piper Dwg. 27972 or Piper Kit 760 705. Flight Manual Supplement Item 401(bz) and placard NOTE 2(x) required on Models PA-24-250 and PA-24-260. Req’d Model PA-24-250, SN 24-1, 24-103 through 24-3687. Req’d Model PA-24-260, SN 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299; 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803; 24-4783, and 24-4804 through 24-5034 (with normally aspirated engine); 24-4783, and 24-4804 through 24-5034 (with turbocharged engine). Removed with Item 618: Modified in accordance with Piper Kit 760 747 (stabilator modification) |
Airplane Flight Manual (Singles) - TCDS Section 401 Full Listing #
| TCDS §401 | Report Number/Name |
|---|---|
| (a) | DMCR Approved Airplane Flight Manual dated June 19, 1957, revised March 7, 1958. Eligible for S/N 24-2 through 24-102 only. |
| (b) | DMCR Approved Airplane Supplement No. 1, revised November 11, 1958, to Airplane Flight Manual Item 401(a). Required when Item 2(a) or 6(a) is installed. |
| (c) | DMCR Approved Airplane Flight Manual dated April 16, 1958. Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-332. |
| (d) | DMCR Approved Airplane Flight Manual dated March 7, 1958. Eligible Model for PA-24, S/N 24-103 through 24-1683 only. |
| (e) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated May 5, 1958, to Airplane Flight Manual for Model PA-24-250, Item 401(c). Required when Item 5(a) is installed. |
| (f) | DMCR Approved Airplane Flight Manual No. 997 dated July 10, 1958. Eligible for Model PA-24-250, S/N 24-1, 24-103 through 24-2002, 24-2004 through 24-2298 only. Required when Item 109(a), (b), (c), or (d) is installed. |
| (g) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated July 10, 1958, revised August 15, 1958, to Airplane Flight Manual No. 997 for Model PA-24-250, Item 401(f). Required when Item 5(a) is installed. |
| (h) | DMCR Approved Airplane Flight Manual Supplement No. 2 dated July 31, 1958, to Airplane Flight Manual No. 997 for Model PA-24-250, Item 401(f). Required when Item 402(a), Piper AutoControl, is installed. |
| (i) | DMCR Approved Airplane Flight Manual Supplement No. 2 dated July 31, 1958, to Airplane Flight Manual for Model PA-24, Item 401(d). Required when Item 402(a), Piper AutoControl, is installed. |
| (j) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated July 31, 1958, to Airplane Flight Manual Supplement No. 973 for Model PA-24-250, Item 401(c). Required when Item 402(a), Piper AutoControl, is installed |
| (k) | DMCR Approved Airplane Flight Manual No. 1047, dated December 11, 1959. Eligible for Model PA-24, S/N 24-1684 through 24-3687 only. Required when Item 111 is installed. |
| (l) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated December 11, 1959, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 2(a) is installed. |
| (m) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated December 11, 1959, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(a) is installed. Revision dated June 28, 1962, required when Course Selector directional gyro is installed. |
| (n) | DMCR Approved Airplane Flight Manual No. 1127, dated September 27, 1960. Eligible for Model PA-24-250, S/N 24-2003, 24-2299 through 24-2562, and 24-2564 through 24-2843 only. Required when Item 112 is installed. |
| (o) | DMCR Approved Airplane Flight Manual Supplement No. 1 dated September 27, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 5(a) is installed. |
| (p) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated September 27, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401 (n). Required when Item 402(a), Piper AutoControl, is installed. |
| (q) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated December 13, 1960, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(b), Piper Altimatic, is installed. |
| (r) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated December 13, 1960, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(b), Piper Altimatic, is installed. |
| (s) | DMCR Approved Airplane Flight Manual No. 1179, dated September 18, 1961. Eligible for Model PA-24-250, S/N 24-2563, 24-2844 through 24-3687, except when Item 109(e) is installed. |
| (t) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated September 18, 1961, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(a), Piper AutoControl, is installed. Revision dated June 28, 1962, required when Course Selector directional gyro is installed. |
| (u) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated September 18, 1961, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(b), Piper Altimatic, is installed. |
| (v) | DMCR Approved Airplane Flight Manual No. 1220, dated February 15, 1962. Eligible for Model PA-24-250, S/N 24-2563, and 24-2844 through 24-3687 only. Required when Item 109(e) is installed. |
| (w) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated February 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(a), Piper AutoControl, is installed with Item 109(e). Revision dated June 28, 1962, required when Course Selector directional gyro is installed. |
| (x) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated February 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(b), Piper Altimatic, is installed with Item 109(e). |
| (y) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 7, 1962, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(c), Piper Altimatic II, is installed. |
| (z) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 7, 1962, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(c), Piper Altimatic II, is installed. |
| (aa) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated August 7, 1962 to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(c), Piper Altimatic II, is installed. |
| (ab) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated August 7, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(c), Piper Altimatic II, is installed with Item 109(e). |
| (ac) | DMCR Approved Airplane Flight Manual Supplement No. 5, dated August 15, 1962, to Airplane Flight Manual No. 1047 for Model PA-24, Item 401(k). Required when Item 402(d), Piper AutoControl II, is installed. |
| (ad) | DMCR Approved Airplane Flight Manual Supplement No. 5, dated August 15, 1962, to Airplane Flight Manual No. 1127 for Model PA-24-250, Item 401(n). Required when Item 402(d), Piper AutoControl II, is installed. |
| (ae) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 15, 1962, to Airplane Flight Manual No. 1179 for Model PA-24-250, Item 401(s). Required when Item 402(d), Piper AutoControl II, is installed. |
| (af) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated August 15, 1962, to Airplane Flight Manual No. 1220 for Model PA-24-250, Item 401(v). Required when Item 402(d), Piper AutoControl II, is installed with Item 109(e). |
| (ag) | DMCR Approved Airplane Flight Manual No. 1295, dated December 27, 1963. Eligible for Model PA-24-400 only. |
| (ah) | DMCR Approved Airplane Flight Manual No. 1333, dated June 19, 1964. Eligible for Model PA-24-260 (Carburetor Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. |
| (ai) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 402(d), Piper AutoControl II, is installed. |
| (aj) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 402(c), Piper Altimatic II, is installed. |
| (ak) | DMCR Approved Airplane Flight Manual No. 1334, dated June 19, 1964. Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299, only. |
| (al) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 402(c), Piper Altimatic II, is installed. |
| (am) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 19, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 420(d), Piper Auto Control II, is installed. |
| (an) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated May 5, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 402(c), Piper Altimatic II, is installed. |
| (ao) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated May 5, 1964, revised July 16, 1964, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 402(d), Piper AutoControl II, is installed. |
| (ap) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 607(a) is installed. |
| (aq) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401(ah). Required when Item 607(a) is installed. |
| (ar) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated February 19, 1965, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 607(a) is installed. |
| (as) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1295, for Model PA-24-400, Item 401(ag). Required when Item 609(a) is installed. |
| (at) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1333, for Model PA-24-260, Item 401 (ah). Required when Item 609(a), Oxygen System, is installed. |
| (au) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated April 30, 1965, to Airplane Flight Manual No. 1334, for Model PA-24-260, Item 401(ak). Required when Item 609(a), Oxygen System, is installed. |
| (av) | DMCR Approved Airplane Flight Manual No. 1358, dated June 30, 1965, revised December 21, 1965, and January 6, 1966. Eligible for Model PA-24-260 (Carburetor Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. |
| (aw) | DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401 (av). Required when Item 402(c), Piper Altimatic II, is installed. |
| (ax) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(d), Piper AutoControl II, is installed. |
| (ay) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 607(a) or 607 (b), Exhaust Gas Temperature Indicator, is installed. |
| (az) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated June 30, 1965, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 609(b), Oxygen System, is installed. |
| (ba) | DMCR Approved Airplane Flight Manual No. 1359, dated June 30, 1965, revised December 21, 1965, and January 6, 1966. Eligible for Model PA-24-260 (Fuel Injection Model), S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803, only. |
| (bb) | [DMCR Approved Airplane Flight Manual Supplement No. 1, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(c), Piper Altimatic II, is installed.][1359_supplement_1] |
| (bc) | DMCR Approved Airplane Flight Manual Supplement No. 2, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(d), Piper AutoControl II, is installed. |
| (bd) | DMCR Approved Airplane Flight Manual Supplement No. 3, dated June 30, 1965, to Airplane Flight Manual No.1359, for Model PA-24-260, Item 401(ba). Required when Item 607(a) or 607(b), Exhaust Gas Temperature Indicator, is installed. |
| (be) | DMCR Approved Airplane Flight Manual Supplement No. 4, dated June 30, 1965, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 609(b), Oxygen System, is installed. |
| (bf) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5, dated May 27, 1966, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(e), Piper AutoControl II (Model AK161), is installed. |
| (bg) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5, dated May 27, 1966, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(e), Piper AutoControl III (Model AK161), is installed. |
| (bh) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 6, dated August 5, 1966, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 402(f), Piper Altimatic III, is installed. |
| (bi) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 6, dated August 5, 1966, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401(ba). Required when Item 402(f), Piper Altimatic III, is installed. |
| (bj) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 7, dated August 7, 1967, to Airplane Flight Manual No. 1358, for Model PA-24-260, Item 401(av). Required when Item 607(c), Exhaust Gas Temperature Indicator, is installed. |
| (bk) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 7, dated August 7, 1967, to Airplane Flight Manual No. 1359, for Model PA-24-260, Item 401 (ba). Required when Item 607(c), Exhaust Gas Temperature Indicator, is installed. |
| (bl) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 1 to Airplane Flight Manual No. 1545. Required when Item 402(g), AutoControl III, is installed. |
| (bm) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 2 to Airplane Flight Manual No. 1545. Required when Item 402(h), Altimatic IIIB, is installed. |
| (bn) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 3 to Airplane Flight Manual No. 1545. Required when Item 609(b), Oxygen System, is installed. |
| (bo) | D.O.A. No. EA-1 Approved Airplane Flight Manual No. 1545, dated April 11, 1969. Eligible for Model PA-24-260, S/N 24-4783, and 24-4804 through 24-5034 only. |
| (bp) | D.O.A. No. EA-1 Approved Airplane Flight Manual No. 1640, dated May 25, 1970. Eligible Model for PA-24-260 (equipped with Turbocharger), S/N 24-4783, and 24-4804 through 24-5034 only. |
| (bq) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 1 to Airplane Flight Manual No. 1640. Required when Item 402(g), AutoControl III, is installed. |
| (br) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 2 to Airplane Flight Manual No. 1640. Required when Item 402(h), Altimatic IIIB, is installed. |
| (bs) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 3 to Airplane Flight Manual No. 1640. Required when Item 609(b), Oxygen System, is installed. |
| (bt) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 4 to Airplane Flight Manual No. 1640. Required when Item 304(c) or 307(a) strobe light is installed. |
| (bu) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 4 to Airplane Flight Manual No. 1545. Required when Item 304(c) or 307(a) strobe light is installed. |
| (bv) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1334. Required when Item 123, Manually Controlled Heated Alternate Engine Induction Air, is installed. |
| (bw) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 8 to Airplane Flight Manual No. 1359. Required when Item 123, Manually Controlled Heated Alternate Engine Induction Air, is installed. |
| (bx) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1545. Required when Item 402(i), Altimatic IIIB1, is installed. |
| (by) | D.O.A. No. EA-1 Approved Airplane Flight Manual Supplement No. 5 to Airplane Flight Manual No. 1640. Required when Item 402(i), Altimatic IIIB1, is installed. |
| (bz) | D.O.A. No. EA-1 approved Airplane Flight Manual Supplement No. 1770 for Models PA-24-250 and PA-24-260 Airplane Flight Manuals dated August 8, 1972, revised September 5 and September 27, 1972. (Copies of Supplement No. 1770 dated August 8, 1972, with no revision date are eligible and approved for use. Copies with two revision dates (September 5 and September 27, 1972) are eligible and approved for use. Copies with only one revision date (September 5, 1972) are not eligible for use.) |