REMOVED REPAIR FRAME STRAP AT B52231 S-17L AS PER SRM 51-40-02. FABRICATED -8 REPAIR FRAME STRAP AT B52231 S-17L AS PER BOEING SR SPI-TLS-26-0017-03B. INSTALLED -8 REPAIR FRAME STRAP AT BS52231 S-17 - [SDR UIEA2026040200121](https://openairdocs.org/sdr/UIEA2026040200121.md): Bulkhead Web · cracked · Mar 29, 2026 · N452PA · Boeing 74746NF · Fuselage Main, Bulkhead > CRACK SIGNAL INDICATION AT L/H AFT INNER CHORD IN ACCORDANCE WITH EO 4453C127 OPEN HOLE HEEL INSPECTION (2EA) REMOVED HI-LOK 10 EA TO PERFORM S.B 747 53A2467 & 53A2427 AT B.S 2598 L/H LOWER BULKHEAD AS PER SPI-TLS-26-0016. PERFORMED OPEN HOLE HFEC INSP AT STA - [SDR UIEA2026040100118](https://openairdocs.org/sdr/UIEA2026040100118.md): Keelbeam · corroded · Mar 29, 2026 · N452PA · Boeing 74746NF · Fuselage Main, Keel > LOWER FUSELAGE STA 1460 KEELBEAM STRUCTURE CORROSION (BETWEEN BOTH BODY L/G DOOR) REMOVED BOTH PANEL AT LWR FUSELAGE BS 1460 KEEL BEAM IAW SRM 51-40-02. PERFORMED BLEND OUT CORROSION AREA AT LWR FUSELAGE BS 1460 KEELBEAM IAW SRM 51-10-02. ACCOMPLISHED FPI IN - [SDR UIEA2025090401161](https://openairdocs.org/sdr/UIEA2025090401161.md): Actuator · faulted · Sep 4, 2025 · N452PA · Boeing 74746NF · Pressure Regulator/Outflow Valve > OUTFLOW VALVE R EICAS MSG. REMOVED & REPLACED RT OUTFLOW VALVE ACTUATOR ASSY, RT ICU & DIODE IAW AMM 21-31-10/401, 21-31-07/401, SWPM 20-40, AIPC 21-31-01-01 & AIPC 21-31-10-01. OPS CHKD OK. - [SDR UIEA2024112001097](https://openairdocs.org/sdr/UIEA2024112001097.md): Fire Warning · false activation · Nov 20, 2024 · N452PA · Boeing 74746NF · Fire Detection > DURING FLIGHT N452PA HAD A MDC FIRE WARNING ALERT. CREW VERIFIED NO FIRE OR SMOKE, CONTINUED TO ANC.(
CONFIRM NO SMOKE OR FIRE FROM PREVIOUS LEG. PERFORMED CARGO DET FIRE TEST PER AMM 26-14-00. NO ACTIVE FAULTS PRESENT.
) - [SDR UIEA2024032100164](https://openairdocs.org/sdr/UIEA2024032100164.md): Smoke Detector · false activation · Mar 21, 2024 · N452PA · Boeing 74746NF · Smoke Detection > CREW REST SMOKE EICAS MSG. NO SMOKE OR FIRE CONFIRMED.(WIRING CHECKED NORMAL PER B747-400 WDM 26-13-31 REV 33. NEED TO REPLACE R/H CREW REST SMOKE DETECTOR. PERFORMED CHECK FLIGHT DECK EQUIPMENT AND CABIN EQUIPMENT. PERFORMED FUMES SMELL CHECK IN BLEED DUCT - [SDR UIEA2024022100096](https://openairdocs.org/sdr/UIEA2024022100096.md): Relay · inoperative · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuel Boost Pump > FOUND R54 RELAY (#4 FWD) GFI RELAY NOT EQUIP(
1) IAW SWPM 20-81-22, 20-20-00 REV. 84, WDM 28-22-31 REV.33 REPLACED #4 FWD GFI RELAY. 2) TRANSFER TO I/C 28-22-03-01 STEP I AND STEP K FOR R54 RELAY TEST AND RESULT WAS SATISFACTORY
) - [SDR UIEA2024022100097](https://openairdocs.org/sdr/UIEA2024022100097.md): Cargo Track · cracked · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485 LBL 75.92(1) PERFORM JOB IAW WORKSHEET #40066 AND DWG #65B38251 SHEET 62 REV A, SHEET 32 REV -, 14440802, SHEET 3 REV B 2) JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024022100099](https://openairdocs.org/sdr/UIEA2024022100099.md): Cargo Track · cracked · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485, RBL 75.92(1) PERFORM JOB IAW WORK SHEET NO: 40068 AND DWG NO:14440802, SHEET 3, REV B, 65B38751, SHEET 62 REV A SHET 32 REV-, SHEET 75 REV- 2) JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024022100100](https://openairdocs.org/sdr/UIEA2024022100100.md): Floorbeam · cracked · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuselage Main, Floor Beam > FND FLOOR STRUCTURE CRACK AT M/D STA 980 RBL 75.92(1) PERFORM JOB IAW WORKSHEET #40071 AND DWG #65B16004, SHEET 4 REV A, 65B38250, SHEET 17 REV A, SHEET 9 REV B 2) JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2024022100101](https://openairdocs.org/sdr/UIEA2024022100101.md): Skin · debonded · Feb 23, 2024 · N452PA · Boeing 74746NF · Spoilers > DISBOND - RH WING #7 SPOILER LWR SURFACE, AT INBD EDGE, T/E EDGE(1) PERFORM INTERIM REPAIR AT #7 SPOILER INBD SIDE T/E AREA, REFER TO EGAT EI T2024A57M-294 REV 1. 2) CONDITION CHECK IS SATISFACTORY
) - [SDR UIEA2024022100102](https://openairdocs.org/sdr/UIEA2024022100102.md): Skin · debonded · Feb 23, 2024 · N452PA · Boeing 74746NF · Ailerons > DISBOND - EDGE, LH WING INBD AILERON OUTBD CORNER.(1) PERFORM REPAIR OF DISBOND SKIN AREA AT LH WING INBD AILERON OUTBD SIDE IAW SRM 57-60-01. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2) CONDITION CHECK IS SATISFACTORY.< - [SDR UIEA2024022100103](https://openairdocs.org/sdr/UIEA2024022100103.md): Skin · chafed · Feb 23, 2024 · N452PA · Boeing 74746NF · Ailerons > CHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE AREA(
1) PERORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2) CONDITION CHECK IS SATISFACTORY.
) - [SDR UIEA2024022100104](https://openairdocs.org/sdr/UIEA2024022100104.md): Floorbeam · none · Feb 23, 2024 · N452PA · Boeing 74746NF · Standard Practices/Structures > DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(1) PERFORM JOB IAW EI T2024A53M-248, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-248, REV-1 3) JOB COMPLETED AND COND CHK NML.
) - [SDR UIEA2024022100105](https://openairdocs.org/sdr/UIEA2024022100105.md): Floorbeam · none · Feb 23, 2024 · N452PA · Boeing 74746NF · Standard Practices/Structures > DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 500 UPPER DECK FLOOR BEAM STRAP HAVE 2 EA FASTENER CAN'T REMOVED.(1) PERFORM JOB IAW EI T2024A53M-249, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-249, REV 1 3) JOB COMPLETED AND COND CHK NML.
) - [SDR UIEA2024022100106](https://openairdocs.org/sdr/UIEA2024022100106.md): Floorbeam · none · Feb 23, 2024 · N452PA · Boeing 74746NF · Standard Practices/Structures > DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT L/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(1) PERFORM JOB IAW EI T2024A53M-246, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-246, REV 1 3) JOB COMPLETED AND COND CHK NML.
) - [SDR UIEA2024022100107](https://openairdocs.org/sdr/UIEA2024022100107.md): Door Frame · cracked · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuselage Main, Structure > FND DOOR CUTOUT CRACK AT L5 DOOR RELEASE HANDLE AREA, STA 2240, WL 250.(1) PERFORM JOB IAW WORK SHEET #40078 2) JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024022100108](https://openairdocs.org/sdr/UIEA2024022100108.md): Cargo Track · cracked · Feb 23, 2024 · N452PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1720 ~ 1730, RBL 75.92(1) PERFORM JOB IAW WORKSHEET #40069 AND DWG #65B38751, SHEET 62 REV A, SHEET 32 REV-, SHEET 75 REV- 2) JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2023090800828](https://openairdocs.org/sdr/UIEA2023090800828.md): Unknown · unknown · Sep 7, 2023 · N452PA · Boeing 74746NF · Hydraulic Power System > #1 HYD QUANTITY DROPPING(LOCATED LEAK OF HYDRAULIC LINE AT STA 900. REPAIRED PER GMM 3.24.1 USING A NEW SECTION OF PIPE AND 2 EA RYNGLOC FITTINGS. PRESSURE TESTED, NIL LEAKS. FITTINGS USED PN: R80101T08. AMM 20-11-05 FOR REFERENCE.
) - [SDR UIEA2023083100821](https://openairdocs.org/sdr/UIEA2023083100821.md): Acm · unknown · Aug 31, 2023 · N452PA · Boeing 74746NF · Cabin Cooling System > BURNING SMELL & VIBRATION ON FINAL. ISOLATED TO PACK 1. NO INDICATIONS, SHUT OFF PACK(PACK 1 PLACED ON DMI 192433 PER MEL 21-51-01-03 & DMI 192434 PER 26-16-01-02-01B (DUE TO PACK 1 INOP). PACK 1 DMI 192433 & FWD LOBE FIRE DETECTION DMI 192434. CHAPTER 5 CO - [SDR UIEA2022040900276](https://openairdocs.org/sdr/UIEA2022040900276.md): Flap · damaged · Apr 7, 2022 · N452PA · Boeing 74746NF · Leading Edge Slat Control System > DURING WALK AROUND, FOUND #7 L/E FLAP VARIABLE CAMBER DAMAGED(
REPLACED #7 L/E FLAP VARIABLE CAMBER PER AMM 27-81-02/401. PERFORMED FLAP OPS AND FCU GROUND TEST OK PER AMM 27-81-00/801.
/) - [SDR P5CA2022022100062](https://openairdocs.org/sdr/P5CA2022022100062.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1778-1800 LBL 33 SEAT TRACK FOUND CORROSION.(
M/D STA 1778-1800 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100044](https://openairdocs.org/sdr/P5CA2022022100044.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 850 - 809 LBL 11.33" SEAT TRACK FOUND CORROSION(M/D STA 805 - 809 LBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE. 1 FIG 101 LIMIT
) - [SDR P5CA2022022100045](https://openairdocs.org/sdr/P5CA2022022100045.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1920 RBL 75.92 SEAT TRACK FOUND CORROSION.(M/D - STA 1920 RBL 75.92 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100046](https://openairdocs.org/sdr/P5CA2022022100046.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1920 RBL 99 SEAT TRACK FOUND CORROSION(M/D - STA 1920 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100047](https://openairdocs.org/sdr/P5CA2022022100047.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1900 RBL 99 SEAT TRACK FOUND CORROSION(M/D - STA 1900 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100048](https://openairdocs.org/sdr/P5CA2022022100048.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > U/D STA 740 LH TENSION TIE AFT CHANNEL STARTING FROM THE FASTENER HOLE RUNNING O/B TO THE EDGE FOUND CRACKED APPROX 3/8" IN LENGTH.(U/D STA 740 LBL 55" TO END OF O/B TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR IS A PERMANENT REP - [SDR P5CA2022022100049](https://openairdocs.org/sdr/P5CA2022022100049.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1880 RBL 99 SEAT TRACK FOUND CORROSION(
M/D - STA 1880 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100050](https://openairdocs.org/sdr/P5CA2022022100050.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1840 RBL 99 SEAT TRACK FOUND CORROSION(M/D - STA 1840 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100051](https://openairdocs.org/sdr/P5CA2022022100051.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1270-1278 RBL 11.33" SEAT TRACK FOUND CORROSION.(M/D STA 1270-1278 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100052](https://openairdocs.org/sdr/P5CA2022022100052.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1820 RBL 99 SEAT TRACK FOUND CORROSION(M/D - STA 1820 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100053](https://openairdocs.org/sdr/P5CA2022022100053.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1777 - 1784 RBL 99 SEAT TRACK FOUND CORROSION(M/D - STA 1777 - 1784 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100054](https://openairdocs.org/sdr/P5CA2022022100054.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1908 RBL 33 SEAT TRACK FOUND CORROSION(M/D - STA 1908 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100055](https://openairdocs.org/sdr/P5CA2022022100055.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1877 RBL 33 SEAT TRACK FOUND CORROSION(M/D - STA 1877 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100056](https://openairdocs.org/sdr/P5CA2022022100056.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1860 RBL 99 SEAT TRACK FOUND CORROSION.(M/D STA 1860 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100057](https://openairdocs.org/sdr/P5CA2022022100057.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1830-1836 RBL 33 SEAT TRACK FOUND CORROSION.(M/D STA 1830-1836 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100058](https://openairdocs.org/sdr/P5CA2022022100058.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1774-1776 RBL 33 SEAT TRACK FOUND CORROSION.(M/D STA 1774-1776 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100059](https://openairdocs.org/sdr/P5CA2022022100059.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1922 LBL 33 SEAT TRACK FOUND CORROSION.(M/D STA 1922 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100060](https://openairdocs.org/sdr/P5CA2022022100060.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1822-1825 LBL 33 SEAT TRACK FOUND CORROSION.(M/D STA 1822-1825 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100061](https://openairdocs.org/sdr/P5CA2022022100061.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D STA 1886-1890 LBL 33 SEAT TRACK FOUND CORROSION.(M/D STA 1886-1890 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100063](https://openairdocs.org/sdr/P5CA2022022100063.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 2196-2198 LBL 11.33 SEAT TRACK FOUND CORROSION(M/D - STA 2196-2198 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT
) - [SDR P5CA2022022100064](https://openairdocs.org/sdr/P5CA2022022100064.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 2117-2120 LBL 11.33 SEAT TRACK FOUND CORROSION(M/D - STA 2117-2120 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT
) - [SDR P5CA2022022100065](https://openairdocs.org/sdr/P5CA2022022100065.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1470-1480 RBL 11.33 SEAT TRACK FOUND CORROSION(M/D - STA 1470-1480 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT
) - [SDR P5CA2022022100066](https://openairdocs.org/sdr/P5CA2022022100066.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Standard Practices/Structures > M/D - STA 1350-1360 RBL 11.33" SEAT TRACK FOUND CORROSION(M/D - STA 1350-1360 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE. 1 FIG 101 LIMIT
) - [SDR P5CA2022022100067](https://openairdocs.org/sdr/P5CA2022022100067.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1410-1418 RBL 11.33 SEAT TRACK FOUND CORROSION(M/D - STA 1410-1418 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.
) - [SDR P5CA2022022100068](https://openairdocs.org/sdr/P5CA2022022100068.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Standard Practices/Structures > M/D STA 1310-1318 RBL 11.33" SEAT TRACK FOUND CORROSION(M/D STA 1310-1318 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT
) - [SDR P5CA2022022100069](https://openairdocs.org/sdr/P5CA2022022100069.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Doors > M/D STA 1290-1298 RBL 11.33" SEAT TRACK FOUND CORROSION(M/D STA 1290-1298 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT
) - [SDR P5CA2022022100070](https://openairdocs.org/sdr/P5CA2022022100070.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > M/D - STA 1337 RBL 11.33 SEAT TRACK FOUND CORROSION(M/D - STA 1337 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT
) - [SDR P5CA2022022200072](https://openairdocs.org/sdr/P5CA2022022200072.md): None · none · Mar 12, 2022 · N452PA · Boeing 74746NF · Fuselage Structure (General) > STA 2231 1EA CRACK WAS FOUND ON REVEAL RUNNING AFT THROUGH THE FASTENER HOLE AND EXTEND TOWARDS THE EDGE(M/D STA 2231 STR 21L - 22L DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3. THIS REPAIR IS A PERMANENT REPAIR AND CATEGORY B REPA Next page: https://openairdocs.org/aircraft/N452PA/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N452PA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N452PA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.