# Service difficulty reports: N7736A

A list on [N7736A](https://openairdocs.org/aircraft/N7736A.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 · 258 reports

- [SDR SWAA2026101999022](https://openairdocs.org/sdr/SWAA2026101999022.md): Seat · out of adjust · Oct 15, 2026 · N7736A · Boeing 7377BD · Passenger Compartment Equipment
  > SEAT 15D WILL NOT STAY UPRIGHT, OKAY TO CONTINUE IAW MEL 25-6-02 SP 1B. SEAT LOCKED UPRIGHT AND IS USABLE REF. LP 3439875
- [SDR SWAA2026101967765](https://openairdocs.org/sdr/SWAA2026101967765.md): Hydrolock · out of adjust · Oct 15, 2026 · N7736A · Boeing 7377BD · Passenger Compartment Equipment
  > 15D SEATBACK WILL NOT STAY IN UPRIGHT IF OCCUPIED. OK TO CONTINUE PER MEL 25-6-01 SP1B. ADJUSTED LOCKING NUTS RECLINE HYDROLOCK TO LOCK SEAT IN UPRIGHT POSITION PER SIP. SEAT IS NOW USABLE.
- [SDR SWAA2026101999040](https://openairdocs.org/sdr/SWAA2026101999040.md): Girt Bar · out of adjust · Oct 13, 2026 · N7736A · Boeing 7377BD · Emergency Equipment
  > R1 DOOR GIRT BAR LOOSE. ADJUSTED GIRT BAR IAW AMM 25-66-01
- [SDR SWAA2026101269883](https://openairdocs.org/sdr/SWAA2026101269883.md): Light · inoperative · Oct 6, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06-960-805.
- [SDR SWAA2026101209695](https://openairdocs.org/sdr/SWAA2026101209695.md): Lamp · inoperative · Sep 26, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE LAMPS FOR EMERGENCY LIGHT AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-04-960-801.
- [SDR SWAA2026100953693](https://openairdocs.org/sdr/SWAA2026100953693.md): Lamp · inoperative · Sep 26, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > MULTIPLE MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. RELAMPED MULTIPLE MAIN CABIN LIGHTS AND PERFROMED SUCCESSFUL OPS CHECK IAW AMM 33-51-00 AND AMM 33-51-03.
- [SDR SWAA2026072091488](https://openairdocs.org/sdr/SWAA2026072091488.md): Battery Pack · failed · Jul 15, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > FWD LEFT ENTRY EMERGENCY BATTERY PACK AT M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026072052339](https://openairdocs.org/sdr/SWAA2026072052339.md): Battery Pack · failed · Jul 15, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > FWD RT SERVICE EMERGENCY BATTERY PACK AT M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026072077792](https://openairdocs.org/sdr/SWAA2026072077792.md): Light · inoperative · Jul 15, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R CABIN OVERWING EXIT LIGHT ASSY IAW AMM 33-21-00.
- [SDR SWAA2026050695904](https://openairdocs.org/sdr/SWAA2026050695904.md): Engine · fire · May 6, 2026 · N7736A · Boeing 7377BD · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL AIRCRAFT BEHIND REPORTED FLAMES FROM NR 2 ENGINE. NO ABNORMAL INDICATIONS ON THE FLIGHT DECK.. INSPECTED NR 2 ENGINE FOR LEAKS WITH OIL PUDDLING NOTED AT THE CENTER PLUG CAVITY. ENGINE VENTS AND DRAINS INSPECTED IAW AMM 71-71-00. AFT SUMP O
- [SDR SWAA2026042787198](https://openairdocs.org/sdr/SWAA2026042787198.md): Crease Beam · corroded · Apr 7, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Structure
  > CORRODED RT CREASE BEAM WEB, BS 827, RBL 67, WL 208. REMOVED & REPLACED THE CREASE BEAM WEB IAW SRM 51-40-02-0G-0, DWG 146A5900, SHEET 71, REV B. AND DWG 146A5900, SHEET 70, REV -.
- [SDR SWAA2026042785989](https://openairdocs.org/sdr/SWAA2026042785989.md): Window Frame · cracked · Apr 2, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Structure
  > F/O NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED ACCOMPLISHED REPAIR NR 1 WINDOW OTBD POST IAW EA 26-153-00937 WIP1 AND WIP2.
- [SDR SWAA2026042785642](https://openairdocs.org/sdr/SWAA2026042785642.md): Crease Beam · corroded · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Structure
  > PASSENGER CABIN, RT CREASE BEAM INNER CHORD, BS 631 - 642, RBL 65, WL 208 CORRODED. REMOVED AND REPLACED THE CREASE BEAM IAW SRM 51-40-02-0G-0, AND DWG 144A5901, REV -.
- [SDR SWAA2026042785638](https://openairdocs.org/sdr/SWAA2026042785638.md): Attach Angle · cracked · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > RIGHT BS 663 UPPER ATTACH ANGLE CRACKED ON VAPOR BARRIER, RBL 8, WL 167.68. CRACK WAS FOUND TO BE OUT OF LIMITS AND ATTACH ANGLE WAS REPAIRED IAW SRM 57-10-10-2R-5.
- [SDR SWAA2026042785639](https://openairdocs.org/sdr/SWAA2026042785639.md): Floor Support · cracked · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 208. REMOVED & REPLACED THE FLOOR SUPPORT. LOCATED & DRILLED THE FLOORBOARD HOLES IAW SRM 51-40-02, SRM 51-40-05, & DWG 143A0060, SHEET 46, REV -.
- [SDR SWAA2026042785640](https://openairdocs.org/sdr/SWAA2026042785640.md): Floor Support · cracked · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT BS 540 LBL 1 WL 208. REMOVED & REPLACED THE FLOOR SUPPORT. LOCATED AND DRILLED FLOOR BOARD PANEL HOLES IAW SRM 51-40-02, SRM 51-40-05, DWG 143A0060, SHEET 46, REV -.
- [SDR SWAA2026042785645](https://openairdocs.org/sdr/SWAA2026042785645.md): Stringer Clip · cracked · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 257 COMMON TO STR 10L. REMOVED AND REPLACED STRINGER CLIP AT BS 257 COMMON TO STR 10L IAW SRM 51-40-02-0G-0 AND DWG 141A0720; REV:A.
- [SDR SWAA2026042785643](https://openairdocs.org/sdr/SWAA2026042785643.md): Strap · corroded · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 686; RBL 71; WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK REMOVED AND TREATED DAMAGE ON STIFFENER AT BS 686; RBL 70-71; WL 202.5 1.0' L X 0.700' W IAW SRM 51-10-
- [SDR SWAA2026042785644](https://openairdocs.org/sdr/SWAA2026042785644.md): Strap · corroded · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 693; RBL 69-71; WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK.
- [SDR SWAA2026042785647](https://openairdocs.org/sdr/SWAA2026042785647.md): Strap · corroded · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 713, RBL 71, WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK.ACTION 2
- [SDR SWAA2026042785417](https://openairdocs.org/sdr/SWAA2026042785417.md): Pin · corroded · Apr 1, 2026 · N7736A · Boeing 7377BD · Horizontal Stabilizer Structure
  > RT HORIZONTAL STAB REAR SPAR MIDDLE FAILSAFE ATTACH PIN WAS PITTED. FAILSAFE ATTACH PIN WILL BE INSTALLED ON TASK CARD TTG8Q002MTQZ STEP 15.
- [SDR SWAA2026042485641](https://openairdocs.org/sdr/SWAA2026042485641.md): Crossbeam · cracked · Apr 1, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Structure
  > PASSENGER CABIN PANEL BREAK AT BS 540, RBL 45 - RBL 65, WL 208, TOP PLATE IS CRACKED. COMPLETED STEP 2 AND UPDATED STEP 1. REMOVED AND REPLACED PASSENGER CABIN BREAK PANEL AT BS 540; RBL 45 - RBL 65, WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5240
- [SDR SWAA2026042784852](https://openairdocs.org/sdr/SWAA2026042784852.md): Rib · cracked · Mar 31, 2026 · N7736A · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB RIB NR 5 THIRD FROM FWD STIFFENER, CRACKED AT LOWER END. REMOVED, REPAIRED, AND REINSTALLED THE NR 5 RIB IAW SRM 55-10-09-2R-5, SRM 51-40-02-0G-0, DWG 182A3001, REV F, DWG 182A1500, REV -, AND DWG 182A2401, REV F.
- [SDR SWAA2026042784840](https://openairdocs.org/sdr/SWAA2026042784840.md): Scuff Plate · cracked · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FORWARD SERVICE DOOR SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFER TO SOPM 20-30-03. WELDED DAMAGED AREA OF SCUFF PLATE. PENETRANT INSPECT THE WELD AREA IA
- [SDR SWAA2026042484847](https://openairdocs.org/sdr/SWAA2026042484847.md): Strap · corroded · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02. RECEIVED NEW FLOOR STRAP ON PO 8
- [SDR SWAA2026042484841](https://openairdocs.org/sdr/SWAA2026042484841.md): Support · corroded · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PLATE BS 727 TO BS 747, LBL 22, WL 156 IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND
- [SDR SWAA2026042484839](https://openairdocs.org/sdr/SWAA2026042484839.md): Scuff Plate · cracked · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FORWARD CARGO BAY FORWARD CORNER SCUFF PLATE PER AMM 53-30-15-2R-1.
- [SDR SWAA2026042484835](https://openairdocs.org/sdr/SWAA2026042484835.md): Scuff Plate · cracked · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE PER AMM 53-60-15-2R-1.
- [SDR SWAA2026042484838](https://openairdocs.org/sdr/SWAA2026042484838.md): Stub Frame · cracked · Mar 30, 2026 · N7736A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK FOUND R1 DOOR STUB FRAME.7' ABOVE SEAL DEPRESSOR BS 291.5 +9 L:.4'. REMOVED DAMAGE FSD STUB FRAME BS 291.5 + 9; LOCATED; DRILLED AND INSTALLED NEW FSD STUB FRAME SECTION LOCATED AT BS 291.5+9; ABOVE SEAL DEPRESSOR SRM 51-40-02-0G-0 AND BOEING DWG 141
- [SDR SWAA2026042784398](https://openairdocs.org/sdr/SWAA2026042784398.md): Panel · debonded · Mar 29, 2026 · N7736A · Boeing 7377BD · Aerodynamic Fairings
  > PANEL 194CR HAS DISBONDS ON OUTER SURFACE. PANEL 194CR WAS REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2026032382414](https://openairdocs.org/sdr/SWAA2026032382414.md): Cover · missing · Mar 22, 2026 · N7736A · Boeing 7377BD · Emergency Lighting
  > LOWER OVERWING EXIT SIGN F/O SIDE MISSING. INSTALLED LIGHT COVER IAW AMM 33-51-04.
- [SDR SWAA2025122654858](https://openairdocs.org/sdr/SWAA2025122654858.md): Lens · missing · Dec 22, 2025 · N7736A · Boeing 7377BD · Emergency Lighting
  > CREW REPORTS EMERGENCY EXIT LENS MISSING ON OVERWING EXIT FO SIDE. INSTALLED EMERGENCY EXIT LENS COVER IAW AMM 33-51-01.
- [SDR SWAA2025102024970](https://openairdocs.org/sdr/SWAA2025102024970.md): Fuse · blown · Oct 16, 2025 · N7736A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY LIGHT BEHIND L2 INOPERATIVE. R & R THE FUSE FROM BATTERY POWER SUPPLY M1673 IAW AMM 33-51-06-960-804. TEST PASSED.
- [SDR SWAA2025100620766](https://openairdocs.org/sdr/SWAA2025100620766.md): Skirt · out of limits · Oct 3, 2025 · N7736A · Boeing 7377BD · Emergency Equipment
  > PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE GIRT SKIRT IN POOR CONDITION. REMOVED AND REPLACED AFT SERVICE DOOR ESCAPE SLIDE PER MT 756-61-06
- [SDR SWAA2025092918567](https://openairdocs.org/sdr/SWAA2025092918567.md): Cover · unsecure · Sep 26, 2025 · N7736A · Boeing 7377BD · Emergency Lighting
  > ROW 12F EMERGENCY EXIT LIGHT COVER WILL NOT STAY ATTACHED TO LIGHT. INSTALLED NEW LIGHT COVER PER AMM 33-51-01.
- [SDR SWAA2025051369467](https://openairdocs.org/sdr/SWAA2025051369467.md): Girt Bar · out of adjust · May 10, 2025 · N7736A · Boeing 7377BD · Emergency Equipment
  > R1 DOOR GIRT BAR RETAINER CLIPS LOOSE; GIT BAR COMING OUT WHEN DOOR OPENED<[01] TIGHTENED RETAINER CLIPS FOR THE GIRT BAR IN REFERENCE TO SIP
- [SDR SWAA2024120673607](https://openairdocs.org/sdr/SWAA2024120673607.md): Door · cracked · Dec 2, 2024 · N7736A · Boeing 7377BD · Galley Doors
  > CRACK IN FWD SERVICE DOOR (R1) FWD SIDE WHERE SEAL MATES. JUST BEHIND UPPER HINGE. CRACK MEASURES.250. REMOVED AND REPLACED 141A8358Y6 (BOX; R1 DOOR UPPER HINGE BOX) PER SRM 51-40-02.
- [SDR SWAA2024120673609](https://openairdocs.org/sdr/SWAA2024120673609.md): Hinge Box · cracked · Dec 2, 2024 · N7736A · Boeing 7377BD · Fuselage, Door Hinge
  > CRACK EXTENDS BEYOND BLENDED AREA WHILE PERFORMING NDT PER EA 24-153-03356 WIP1 FOUND CRACK TO EXTEND APROX..125' BEYOND BLENDED AREA.<[01] REMOVED AND REPLACED 141A8358Y6 (BOX; R1 DOOR UPPER HINGE BOX) PER SRM 51-40-02 COMPLETED ON FAULT NO: TTG8Q00XDE61
- [SDR SWAA2024111860983](https://openairdocs.org/sdr/SWAA2024111860983.md): Slide · out of position · Nov 17, 2024 · N7736A · Boeing 7377BD · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE FELL OUT OF CONTAINER BUT DID NOT DEPLOY<[01] REMOVE AND REPLACE FORWARD ENTRY DOOR SLIDE I.A.W. 25-66-01 OK FOR SERVICE
- [SDR SWAA2024081425799](https://openairdocs.org/sdr/SWAA2024081425799.md): Seat · misconfigured · Aug 14, 2024 · N7736A · Boeing 7377BD · Passenger Compartment Equipment
  > SEAT 11B & 11C RECLINING INTO OVERWING EXIT ROW<[01] LOCKED OUT SEATS 11B AND 11C PER AMM 25-22-00.
- [SDR SWAA2024052287850](https://openairdocs.org/sdr/SWAA2024052287850.md): Slide · dislodged · May 19, 2024 · N7736A · Boeing 7377BD · Escape Slide
  > FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE DISLODGED WHEN DOOR OPENED. GIRT BAR WAS NOT ENGAGED; SLIDE WAS NOT ACTIVATED.<[01] RE INSTALLED FWD SERVICE DOOR ESCAPE SLIDE PACK AND COVER PER AMM 25-66-01. OP CHECK GOOD.
- [SDR SWAA2024052086045](https://openairdocs.org/sdr/SWAA2024052086045.md): Lamp · inoperative · May 15, 2024 · N7736A · Boeing 7377BD · Emergency Lighting
  > INOP LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA 2024-259404<[01] REPLACED LAMPS IN LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW B737-700 AMM 33-51-00-710-801<BR>TEST I
- [SDR SWAA2024051578352](https://openairdocs.org/sdr/SWAA2024051578352.md): Stub Frame · cracked · Apr 23, 2024 · N7736A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK INDICATION IN HOLE FROM STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. LOOKING FWD CRACK DIRECTION IS: 7 O CLOCK. 2024-259366 CRACK ON WEB LOCATED BTW BS 291.5 TO BS 340 AT LEVEL STR 17R AT FWD GALLEY AREA SEE PICTURES ON TASK INFORMATI
- [SDR SWAA2024052084498](https://openairdocs.org/sdr/SWAA2024052084498.md): Angle · perforated · Apr 17, 2024 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > PERFORATION ON ANGLE LOCATED BS540 PLUS 8INCH AND RBL41 AT AIR CONDITIONING BAY 2024-259288<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED BS540 TO 540+13? AND RBL41 AT AIR CONDITIO
- [SDR SWAA2024052076303](https://openairdocs.org/sdr/SWAA2024052076303.md): Bracket · cracked · Apr 17, 2024 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY 2024-259286<[01] REPLACED BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540
- [SDR SWAA2024052076304](https://openairdocs.org/sdr/SWAA2024052076304.md): Bracket · cracked · Apr 17, 2024 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY 2024-259287<[01] REPLACED BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540
- [SDR SWAA2024051676300](https://openairdocs.org/sdr/SWAA2024051676300.md): Angle · cracked · Apr 17, 2024 · N7736A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING 2024-259282<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING TOOK MEASURE OF CRACK IS 0.835 INCH TOOL USED CALIPER P/N: 500-196-30 S/N: A22
- [SDR SWAA2024051676302](https://openairdocs.org/sdr/SWAA2024051676302.md): Plate · cracked · Apr 17, 2024 · N7736A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING 2024-259283<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; MEASURED CRACK IS L: 0.799 INCH TOOL USED CALIPER P/N: 8647A4
- [SDR SWAA2024051576306](https://openairdocs.org/sdr/SWAA2024051576306.md): Light · broken · Apr 17, 2024 · N7736A · Boeing 7377BD · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE 2024-259291<[01] REPLACED EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE IAW B737-700 AMM 33-51-03-960-802; STEP 3.D. (1); EXCEPT 3.D. (1) (A) AND (I).;[02] REPLACED EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE IAW B
- [SDR SWAA2024052075514](https://openairdocs.org/sdr/SWAA2024052075514.md): Angle · cracked · Apr 16, 2024 · N7736A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-259235<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 149A8103 SHEET: 7 REV: A; SEE INDIVI

Next page: https://openairdocs.org/aircraft/N7736A/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 = 'N7736A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7736A/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.