# Service difficulty reports: N262WN

A list on [N262WN](https://openairdocs.org/aircraft/N262WN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 272 reports

- [SDR SWAA2026061612672](https://openairdocs.org/sdr/SWAA2026061612672.md): Battery Pack · no test · Jun 16, 2026 · N262WN · Boeing 7377H4 · Emergency Lighting
  > THE AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026030274904](https://openairdocs.org/sdr/SWAA2026030274904.md): Cover · damaged · Feb 27, 2026 · N262WN · Boeing 7377H4 · Escape Slide
  > AFT L2 ENTRY DOOR SLIDE COVER TRIM MISSING AT AFT END. REPLACED AFT L2 ENTRY DOOR SLIDE COVER TRIM, AFT END IAW AMM 25-66-00.
- [SDR SWAA2025110330559](https://openairdocs.org/sdr/SWAA2025110330559.md): Fan · odor · Oct 31, 2025 · N262WN · Boeing 7377H4 · Air Distribution Fan
  > ODOR IN CABIN WITH CONDITIONED AIR HOOKED UP. TROUBLESHOT AND FOUND RECIRC FAN INOPERATIVE. OK TO CONTINUE PER MEL MEL 21-31-02. REMOVED & REPLACED THE RECIRC FAN IAW AMM 21-25-02 OPS TEST GOOD.
- [SDR SWAA2025100320417](https://openairdocs.org/sdr/SWAA2025100320417.md): Battery Pack · failed · Oct 2, 2025 · N262WN · Boeing 7377H4 · Emergency Lighting
  > AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025082105520](https://openairdocs.org/sdr/SWAA2025082105520.md): Vapor Barrier · cracked · Aug 18, 2025 · N262WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FOUND EIGHT CRACKS ON AFT SIDE OF VAPOR BARRIER IN WHEEL WELL FORWARD SIDE, RBL 32 TO RBL 37, WL 154. SEE TTG8Q014MD18 FOR WORK PERFORMED.
- [SDR SWAA2025082105521](https://openairdocs.org/sdr/SWAA2025082105521.md): Vapor Barrier · cracked · Aug 18, 2025 · N262WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FOUND THREE CRACKS ON AFT SIDE OF VAPOR BARRIER. RBL 45 TO RBL 48, WL 157. SEE TTG8Q014MD0A FOR WORK PERFORMED.
- [SDR SWAA2025072393265](https://openairdocs.org/sdr/SWAA2025072393265.md): Sign · detached · Jul 20, 2025 · N262WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT SIDE OVER WING EMERGENCY EXIT SIGN HAS COME OFF. RESECURED RT OVER WING EMERGENCY EXIT SIGN PER AMM 33-51-01.
- [SDR SWAA2025010883944](https://openairdocs.org/sdr/SWAA2025010883944.md): Battery Pack · no test · Jan 8, 2025 · N262WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN; BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1675 IAW AMM 33-51-06.
- [SDR SWAA2024111960642](https://openairdocs.org/sdr/SWAA2024111960642.md): Apu · shutdown · Nov 16, 2024 · N262WN · Boeing 7377H4 · Airborne Auxiliary Power Unit (APU) System
  > APU AUTO SHUTDOWN IN CRUISE AND WOULD NOT COME BACK ONLINE 11/12-SMOKE COMING FROM TAILPIPE-REPLACED OIL COOLER 11/8-SERVICED APU GEARBOX OPS CHECKED OK 11/2-REPLACED LUBE UNIT FILTER AND START/GEN FILTER OPS CHECKS OK 11/2-SMOKE COMING FROM TAILPIPE-R/R'D OIL
- [SDR SWAA2024110656041](https://openairdocs.org/sdr/SWAA2024110656041.md): Apu · smoke · Nov 2, 2024 · N262WN · Boeing 7377H4 · APU Core Engine
  > APU BLOWING BLACK SMOKE OUT OF EXHAUST<[01] WORKING MEL 49-1-01 SP #1 FROM THIS L/P 2803726. PERFORMED FIM 49-55 TASK 801. OPS CK GOOD. NO SMOKE NOTICED FROM APU EXHAUST.
- [SDR SWAA2024082627810](https://openairdocs.org/sdr/SWAA2024082627810.md): Slide · out of position · Aug 19, 2024 · N262WN · Boeing 7377H4 · Escape Slide
  > CUSTOMER REQUEST PAX CABIN AFT LEFT AND RIGHT DOORS SLIDES RUBBING AGAINST TO SCUFF PLATE STRUCTURE TO CLOSE POSITION 2024-421164<[01] CORRECTED INSTALLED PAX CABIN AFT LEFT AND RIGHT DOORS SLIDES RUBBING AGAINST TO SCUFF PLATE STRUCTURE TO CLOSE POSITION IAW
- [SDR SWAA2024082622737](https://openairdocs.org/sdr/SWAA2024082622737.md): Gate · cracked · Aug 5, 2024 · N262WN · Boeing 7377H4 · Galley Doors
  > CRACK LOWER ENDGATE FWD SERVICE DOOR AT FWD GALLEY AREA 2024-421134<[01] REPLACED LOWER ENDGATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 52-41-61-400-801.<BR>SEE INDIVIDUAL SINGOFF BELOW;[02] REPLACED LOWER ENDGATE FWD SERVICE DOOR AT FWD GALLEY AR
- [SDR SWAA2024082615393](https://openairdocs.org/sdr/SWAA2024082615393.md): Stringer · cracked · Jul 22, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER U8 INTERNAL AREA FUEL TANK UPPER POSITION LOCATED BTW RIB 19 AND RIB 20 AT RT WING 2024-421114<[01] REPAIRED STRINGER U8 INTERNAL AREA FUEL TANK UPPER POSITION LOCATED BTW RIB 19 AND RIB 20 AT RT WING IAW EA 24-157-02096 [TTG8Q00V61GE] AND EA 24
- [SDR SWAA2024082616255](https://openairdocs.org/sdr/SWAA2024082616255.md): Balance Weight · out of balance · Jul 15, 2024 · N262WN · Boeing 7377H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE OF ELEVATOR LT P/N: 183A0103-21 FOUND BALANCE WEIGHTS P/N: 183A0210-15 (1EA) ON BAY 4; P/N: 183A0210-14 (1EA) ON BAY 3; P/N: 183A0210-14 (1EA) ON BAY 2 THIS BALANCE WEIGHTS. 2024-421078<[01] MULTI-EFFECTIVE EA M-22-155-03767 (TCO-SWA-
- [SDR SWAA2024082612915](https://openairdocs.org/sdr/SWAA2024082612915.md): Web · damaged · Jul 15, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE LOCATED ON WEB LOWER AREA VAPOR BARRIER R/H SIDE RBL 6.15 AND RBL 31.83 2024-421088<[01] REPLACED WEB LOCATED LOWER AREA VAPOR BARRIER R/H SIDE RBL 6.15 AND RBL 31.83 IAW B737-700 SRM 51-10-02 AND DWG 111A1511; SHEET 25; REV: -;[02] CORRECTED ST
- [SDR SWAA2024082612914](https://openairdocs.org/sdr/SWAA2024082612914.md): Bracket · cracked · Jul 15, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BRACKET LOCATED ON VAPOR BARRIER R/H SIDE RBL 45 AND RBL 54.21 2024-421087<[01] REPLACED BRACKET LOCATED ON VAPOR BARRIER R/H SIDE RBL 45 AND RBL 54.21 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 11A1001 SHEET 378 REV:A SEE INDIVIDUAL SIGN OFF BELOW.<BR>INS
- [SDR SWAA2024082612117](https://openairdocs.org/sdr/SWAA2024082612117.md): Angle · damaged · Jul 13, 2024 · N262WN · Boeing 7377H4 · Passenger/Crew Doors
  > ELONGATE HOLE ON Z ANGLE (2 EA) LOC. ON LH FWD ENTRY DOOR AT LEVEL LBL 53 PASSENGER CABIN 2024-421055<[01] REPLACED ON Z ANGLE (2 EA) LOC. ON LH FWD ENTRY DOOR AT LEVEL LBL 53 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0;[02] COR
- [SDR SWAA2024082612113](https://openairdocs.org/sdr/SWAA2024082612113.md): Stub Frame · cracked · Jul 13, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED ON BS 294.5 LOCATED BTW STR S-8R TO S- 9R AT PASSENGER CABIN 2024-421058<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-7R AND STR-10R FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM B737-700
- [SDR SWAA2024082612116](https://openairdocs.org/sdr/SWAA2024082612116.md): Angle · cracked · Jul 13, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 272 AT RT WING 2024-421061<[01] REPLACED ANGLE TRAILING EDGE ORSS 272 AT RT WING <BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02;[02] REPLACED ANGLE TRAILING EDGE ORSS 272 AT RT WING <BR>IAW B737-700 SRM 51-10-02 I
- [SDR SWAA2024082612119](https://openairdocs.org/sdr/SWAA2024082612119.md): Support · corroded · Jul 13, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AILERON FEEL AND CENTERING UNIT REACTION SUPPORT AT MAIN WHEEL WELL COMPARTMENT 2024-421064<[01] REPLACED AILERON FEEL AND CENTERING UNIT REACTION SUPPORT AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 CMM 27-14-22.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02]
- [SDR SWAA2024082611845](https://openairdocs.org/sdr/SWAA2024082611845.md): Lens · broken · Jul 12, 2024 · N262WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA (1EA) 2024-421050<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3. C. (7) ITEM (10);[02] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA I
- [SDR SWAA2024082612112](https://openairdocs.org/sdr/SWAA2024082612112.md): Bracket · cracked · Jul 12, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK BRACKET LOCATED BS540 PLUS 8INCH AND RBL10 AT AIR CONDITIONING BAY 2024-421054<[01] REPLACED BRACKET LOCATED BS540 PLUS 8INCH AND RBL10 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02; AND MEASUR
- [SDR SWAA2024082611503](https://openairdocs.org/sdr/SWAA2024082611503.md): Angle · cracked · Jul 11, 2024 · N262WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-421002<[01] REPLACED ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2710; SHEET 8; REV: A. MEASURE OF CRACK IS L:0.462?; TOOL USED
- [SDR SWAA2024082610796](https://openairdocs.org/sdr/SWAA2024082610796.md): Shield · corroded · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 480 TO BS 500 AT LEVEL STR 26R WL 156.1 AT FWD CARGO COMPARTMENT 2024-420944<[01] REPLACED SHIELD WEB LOCATED BTW BS 480 TO BS 500 AT LEVEL STR 26R WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143
- [SDR SWAA2024082610959](https://openairdocs.org/sdr/SWAA2024082610959.md): Lens · broken · Jul 9, 2024 · N262WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LENS ASSY EMERGENCY LIGHT IN LAVATORY B AT AFT GALLEY AREA 2024-420973<[01] REPLACED LENS ASSY EMERGENCY LIGHT IN LAVATORY B AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802. PERFORMED TEST IS OK.;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2024082610957](https://openairdocs.org/sdr/SWAA2024082610957.md): Stringer · corroded · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 23L LOCATED BS 540 WL 155 FWD CARGO COMPARTMENT 2024-420954<[01] ON STEP 9; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DA
- [SDR SWAA2024082610793](https://openairdocs.org/sdr/SWAA2024082610793.md): Angle · cracked · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE LOATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT 2024-420924<[01] REPLACED GUSSET ANGLE AND FASTENERS LOC. BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174 R
- [SDR SWAA2024082610789](https://openairdocs.org/sdr/SWAA2024082610789.md): Angle · cracked · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2024-420931<[01] REPLACED GUSSET ANGLE AND FASTENERS LOC. BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174
- [SDR SWAA2024082610955](https://openairdocs.org/sdr/SWAA2024082610955.md): Support Angle · cracked · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-420951<[01] REPLACED SUPPORT ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B7
- [SDR SWAA2024082610958](https://openairdocs.org/sdr/SWAA2024082610958.md): Support Bracket · cracked · Jul 9, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-420955<[01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWIN
- [SDR SWAA2024082610551](https://openairdocs.org/sdr/SWAA2024082610551.md): Strap · corroded · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BTW BS 767 TO BS 787 AND BTW RBL13.84 TO LBL 17.24 WL 156.1 AT AFT CARGO COMPARTMENT 2024-420866<[01] REPLACED STRAP LOCATED BTW BS 767 TO BS 787 AND BTW RBL13.84 TO LBL 17.24 WL 156.1 AT AFT CARGO COMPARTMENT.IAW B737-700 SRM 51-40-02-
- [SDR SWAA2024082610347](https://openairdocs.org/sdr/SWAA2024082610347.md): Support Angle · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 26R AFT POSITION AT AFT CARGO COMPARTMENT 2024-40848<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 26R AFT POSITION AT AFT CARGO COMPARTM
- [SDR SWAA2024082610356](https://openairdocs.org/sdr/SWAA2024082610356.md): Support Bracket · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SPPORT BRACKET LOCATED PARTITION BS 727 BTW RBL 3 TO LBL 3 AT AFT CARGO COMPARTMENT 2024-420863<[01] REPLACED SUPPORT BRACKET LOCATED PARTITION BS 727 BTW RBL 3 TO LBL 3 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG: 144A260
- [SDR SWAA2024082610555](https://openairdocs.org/sdr/SWAA2024082610555.md): Support Angle · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 727 PLUS 4 INCHES BTW STR 25R TO STR 25L AT AFT CARGO COMPARTMENT 2024-420885<[01] REPLACED SUPPORT ANGLE LOCATED BS 727 PLUS 4 INCHES BTW STR 25R TO STR 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. <BR>SEE I
- [SDR SWAA2024082610556](https://openairdocs.org/sdr/SWAA2024082610556.md): Support Angle · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INTERNAL STRUCTURE SUPPORT ANGLE LOCATED CEILING AREA BTW BS 847 TO BS 867 AT RBL 46 AT AFT CARGO COMPARTMENT 2024-420888<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BTW BS 847 TO BS 867 AT RBL 46 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02
- [SDR SWAA2024082610354](https://openairdocs.org/sdr/SWAA2024082610354.md): Cargo Track · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK LBL 17.24 LOCATED BS 767 AT AFT CARGO COMPARTMENT 2024-420861<[01] TOOL USED STEP 4 AND 5 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 220272712 DUE DATE: 28-NOV-24;[02] REPAIRED TRACK LBL 17.24 LOCATED BTW BS 747 + 11.5? AND BS 767 + 9.5? AT AFT
- [SDR SWAA2024082610350](https://openairdocs.org/sdr/SWAA2024082610350.md): Cargo Track · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK RBL 13.84 LOCATED BS 767 AT AFT CARGO COMPARTMENT 2024-420850<[01] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.;[02] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.
- [SDR SWAA2024082610348](https://openairdocs.org/sdr/SWAA2024082610348.md): Cargo Track · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK RBL 13.84 LOCATED BS 747 AT AFT CARGO COMPARTMENT 2024-420852<[01] 'REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.';[02] 'REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.'
- [SDR SWAA2024082610351](https://openairdocs.org/sdr/SWAA2024082610351.md): Cargo Track · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK RBL 13.84 LOCATED BS 727C AT AFT CARGO COMPARTMENT 2024-420855<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] ON STEP 10: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 14 APR 25.;
- [SDR SWAA2024082610349](https://openairdocs.org/sdr/SWAA2024082610349.md): Cargo Track · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK RBL 13.84 LOCATED BS 727E AT AFT CARGO COMPARTMENT 2024-420853<[01] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.;[02] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.
- [SDR SWAA2024082610346](https://openairdocs.org/sdr/SWAA2024082610346.md): Fitting · cracked · Jul 8, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-20847<[01] REPLACED FITTING AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-4
- [SDR SWAA2024082610227](https://openairdocs.org/sdr/SWAA2024082610227.md): Stub Frame · cracked · Jul 7, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-420826<[01] TOOL USED ON STEP 5 AND 6: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25;[02] REPAIRED STUB FRAME LOCATED ON BS 294.5 AT LEVEL STR 17R AT F
- [SDR SWAA2024082610109](https://openairdocs.org/sdr/SWAA2024082610109.md): Tie Clip · cracked · Jul 7, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-420817<[01] REPLACED TIE CLIP LOC. BS277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET: 18 REV.- AND DWG 141A8380 SHEET 21 REV.-<
- [SDR SWAA2024082610108](https://openairdocs.org/sdr/SWAA2024082610108.md): Intercostal · cracked · Jul 7, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2024-420815<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B
- [SDR SWAA2024082610106](https://openairdocs.org/sdr/SWAA2024082610106.md): Frame · cracked · Jul 7, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-420816<[01] REPAIRED FRAME LOCATED STA 312 BTW STR5L TO STR6L FWD GALLEY AREA IAW EA NO M-22-153-01244 REV B. SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPAIRED FRAME LOCATED STA 312 BTW STR
- [SDR SWAA2024082609962](https://openairdocs.org/sdr/SWAA2024082609962.md): Support Angle · cracked · Jul 6, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN 2024-420799<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 A
- [SDR SWAA2024082609964](https://openairdocs.org/sdr/SWAA2024082609964.md): Support Angle · cracked · Jul 6, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN 2024-420801<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-
- [SDR SWAA2024082609963](https://openairdocs.org/sdr/SWAA2024082609963.md): Support Angle · cracked · Jul 6, 2024 · N262WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN 2024-420802<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-
- [SDR SWAA2024082609805](https://openairdocs.org/sdr/SWAA2024082609805.md): Bear Strap · cracked · Jul 6, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BS 290-296 BETWEEN S-8R AND S-9R AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.125 INCH 2024-420774<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7 AND 8. THE DIGITAL CAL
- [SDR SWAA2024082609807](https://openairdocs.org/sdr/SWAA2024082609807.md): Floorbeam · corroded · Jul 6, 2024 · N262WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-420778<[01] FLOR BEAM UPPER SURFACE LOCATED BS 986.5 LBL43 AFT GALEY AREA MUST BE REPAIR DUE TO CORROSION EXCEED ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-70-51-1A-1 ALLOWABLE D

Next page: https://openairdocs.org/aircraft/N262WN/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 = 'N262WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N262WN/reports

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