# Service difficulty reports: N7887A

A list on [N7887A](https://openairdocs.org/aircraft/N7887A.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 5 · 231 reports

- [SDR SWAA2026102696228](https://openairdocs.org/sdr/SWAA2026102696228.md): Acoustic Panel · delaminated · Oct 20, 2026 · N7887A · Boeing 737752 · Turbine Engine Air Inlet Section
  > NR 2 ENGINE ACOUSTIC PANEL NR 6 WAS DELAMINATED. REMOVED & REPLACED THE ACCOUSTIC PANEL ON NR 2 ENGINE IAW AMM 72-23-02.
- [SDR SWAA2026101970438](https://openairdocs.org/sdr/SWAA2026101970438.md): Seat · loose · Oct 15, 2026 · N7887A · Boeing 737752 · Passenger Compartment Equipment
  > SEAT ROW LOOSE AT 15FED REMOVED AND REINSTALLED SEAT ROW 15FED IAW AMM 25-22-00-401-NG T.W:K01112 CAL:17DEC2025 DUE:31DEC2026 VERIFIED REMOVED AND REINSTALLED SEAT ROW 15FED IAW AMM 25-22-00-401-NG T.W:K01112 CAL:17DEC2025 DUE:31DEC2026
- [SDR SWAA2026101910270](https://openairdocs.org/sdr/SWAA2026101910270.md): Bracket · loose · Oct 13, 2026 · N7887A · Boeing 737752 · Emergency Equipment
  > FWD MEGAPHONE BRACET LOOSE FAULT. SECURED THE BRACKET IAW SIP.
- [SDR SWAA2026090759588](https://openairdocs.org/sdr/SWAA2026090759588.md): Compressor · stalled · Sep 4, 2026 · N7887A · Boeing 737752 · Turbine Engine Compressor Section
  > DURING CLIMB, NR 1 ENGINE COMPRESSOR STALLED 4 TIMES IN RAPID SUCCESSION WITH LOSS OF N1 INDICATION. NORMAL ENGINE OPS AFTER COMPLYING WITH QRH. PERFORMED BOROSCOPE INSPECTION & INSPECTION OF THE ENGINE AFTER AN ENGINE STALL PROCEDURE IAW MM 71-00-00-210-801
- [SDR SWAA2026012363442](https://openairdocs.org/sdr/SWAA2026012363442.md): Door · cracked · Jan 22, 2026 · N7887A · Boeing 737752 · Landing Gear Doors
  > LEFT MLG CENTER DOOR HAD A CRACK ON LOWER FWD SECTION. REMOVED CENTER AND INNER DOOR ON LT GEAR REFORM MM 32-13-11 OK TO CONT REF AUTH 302986 AND CDL 32-10-03.
- [SDR SWAA2025081299948](https://openairdocs.org/sdr/SWAA2025081299948.md): Control Unit · faulted · Aug 8, 2025 · N7887A · Boeing 737752 · Overheat Detection
  > LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED TWICE ON TAXI OUT. R & R COMPARTMENT OVERHEAT DETECTION CONTROL UNIT IN REF TO AMM 26-18-01. NO CURRENT FAULTS
- [SDR SWAA2025081199949](https://openairdocs.org/sdr/SWAA2025081199949.md): Fire Detector · false activation · Aug 8, 2025 · N7887A · Boeing 737752 · Fire Detection
  > WHEEL WELL FIRE LIGHT AT THE HOLD SHORT JUST BEFORE TAKEOFF.LIGHT REMAINED ON. CRASH FIRE AND RESCUE VERIFIED NO INDICATIONS OF FIRE OR SMOKE WITH ENGINES SHUT DOWN. STARTED ENGINE 2 AND RETURNED TO GATE FIRE WARNING VERBAL. ALARM SET OFF EACH TIME ELECTRICAL
- [SDR SWAA2025073095524](https://openairdocs.org/sdr/SWAA2025073095524.md): Handle · loose · Jul 26, 2025 · N7887A · Boeing 737752 · Service Doors
  > FWD GALLEY AREA R1 DOOR ASSISTANCE HANDLE LOOSE. INSTALLED CORRECTLY FWD GALLEY AREA R1 DOOR ASSISTANCE HANDLE IAW AMM 52-41-31-400-802 STEP 3F(2).
- [SDR SWAA2025072988571](https://openairdocs.org/sdr/SWAA2025072988571.md): Access Panel · damaged · Jul 5, 2025 · N7887A · Boeing 737752 · Vertical Stabilizer, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 323CL AT VERTICAL STABILIZER. REPLACED ACCESS PANEL 323CL AT VERTICAL STABILIZER IAW B737-700 DWG 172A6120 SHEET 1 REV. F.
- [SDR SWAA2025072987754](https://openairdocs.org/sdr/SWAA2025072987754.md): Floorbeam · cracked · Jul 2, 2025 · N7887A · Boeing 737752 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR STRUCTURE SUPPORT LOCATED BS 540 AND BTW BL 0 TO RBL 24.75 AT MAIN CABIN. REPLACED BREAK PANEL AND FASTENERS LOCATED BS 540 AND BTW BL 0 TO RBL 24.75 AT MAIN CABIN IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 143A0060 SHEET: 46 REV -.
- [SDR SWAA2025073087176](https://openairdocs.org/sdr/SWAA2025073087176.md): Angle · cracked · Jul 1, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK ON ANGLE TRAILING EDGE LOCATED AREA DEFLECTION CONTROL RIB ORSS278 RT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED AREA DEFLECTION CONTROL RIB ORSS278 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A6200; SHEET 11; REV B.
- [SDR SWAA2025072987175](https://openairdocs.org/sdr/SWAA2025072987175.md): Plate · cracked · Jul 1, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS327 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS327 AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9, AND DWG 115A3700 SHEET: 41 REV -.
- [SDR SWAA2025073086808](https://openairdocs.org/sdr/SWAA2025073086808.md): Support Bracket · cracked · Jun 30, 2025 · N7887A · Boeing 737752 · Trailing Edge Flaps
  > CRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS 273 LT WING/ REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS 273 LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2930, SHEET 7, REV-.
- [SDR SWAA2025073086807](https://openairdocs.org/sdr/SWAA2025073086807.md): Angle · cracked · Jun 30, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK ANGLE ON TRAILING EDGE LOCATED ON AREA DEFLECTION CONTROL RIB ORSS278 LT WING. REPLACED ANGLE ON TRAILING EDGE LOCATED ON AREA DEFLECTION CONTROL RIB ORSS278 LT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A6200; SHEET: 11; REV: B.
- [SDR SWAA2025073087039](https://openairdocs.org/sdr/SWAA2025073087039.md): Support Bracket · cracked · Jun 30, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE IRSS141 LT WING. REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE IRSS141 LT WING IAW. B737-700 SRM 51-40-02 AND DWG 115A2000 SHEET 21 REV-; MEASURES CRACK IS 1.434 INCHES.
- [SDR SWAA2025073086242](https://openairdocs.org/sdr/SWAA2025073086242.md): Support Angle · cracked · Jun 28, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW. SRM 51-40-02 MEASURES OF CRACK IS 1.124 INCHES.
- [SDR SWAA2025072986452](https://openairdocs.org/sdr/SWAA2025072986452.md): Web · cracked · Jun 28, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BTW BS927 TO BS947.5 AND RBL21 AT AFT CARGO COMPARTMENT INSTALLED WEB-INTERCOSTAL AND FASTENERS LOCATED BTW BS927 TO BS947.5 AND RBL21 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 147A7500 SHEET 27 REV-.
- [SDR SWAA2025072986450](https://openairdocs.org/sdr/SWAA2025072986450.md): Support Angle · cracked · Jun 28, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW S25R TO S27R AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE BETWEEN BS 907 TO BS 927 STR 25R AND STR 27R AT AFT CARGO COMPARTMENT IAW SRM 51-10-02-0G, PARAGRAPH 9, SRM 51-40-02-0G, AND DWG 147A7221, SHEET 24,
- [SDR SWAA2025072986451](https://openairdocs.org/sdr/SWAA2025072986451.md): Support Bracket · cracked · Jun 28, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS947.5 AND LBL11 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02, SRM 51-10-02, AND DWG 149A8103, SHEET 7, REV A.
- [SDR SWAA2025073085414](https://openairdocs.org/sdr/SWAA2025073085414.md): Web · cracked · Jun 25, 2025 · N7887A · Boeing 737752 · Wing Main, Frame Structure
  > CRACK ON WEB LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT LT WING. REPLACED WEB LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT LT WING IAW SRM 51-10-02, SRM 51-40-02, DWG: 115A2512, SHEET 14, REV A.
- [SDR SWAA2025073085415](https://openairdocs.org/sdr/SWAA2025073085415.md): Angle · cracked · Jun 25, 2025 · N7887A · Boeing 737752 · Wing Miscellaneous Structure
  > CRACK ON ANGLE LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT RT WING. REPLACED WEB AND FASTENERS LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A2900, SHEET 1, REV E.
- [SDR SWAA2025072985416](https://openairdocs.org/sdr/SWAA2025072985416.md): Floorbeam · corroded · Jun 25, 2025 · N7887A · Boeing 737752 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AND RBL 43 WL 208.1 AT AFT GALLEY AREA. PERFORMED REPAIR FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AND RBL 43 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6 REPAIR 6.
- [SDR SWAA2025072984627](https://openairdocs.org/sdr/SWAA2025072984627.md): Web · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BS 294.5 TO BS303.9 AND S-16L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR CATEGORY B ON WEB LOCATED BS 294.5 TO BS303.9 AND S-16L AT PASSENGER CABIN IAW EA 25-153-01804-WIP1 AND EA 25-153-01804.
- [SDR SWAA2025072984620](https://openairdocs.org/sdr/SWAA2025072984620.md): Floorbeam · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Main, Floor Beam
  > CRACK FLOORBEAM LOCATED BS 294.5 AND RBL 52 FWD GALLEY AND LAV. PERFORMED PERMANENT REPAIR CAT A; FLOOR BEAM LOCATED BS 294.5; BTW RBL 20 TO RBL 60 IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16.
- [SDR SWAA2025072984625](https://openairdocs.org/sdr/SWAA2025072984625.md): Floor Support · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT LOCATED BS312 TO BS 328 AND LBL 46, FWD GALLEY AND LAV REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.
- [SDR SWAA2025072984621](https://openairdocs.org/sdr/SWAA2025072984621.md): Floor Support · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV. REPLACED WEB INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHE
- [SDR SWAA2025072984624](https://openairdocs.org/sdr/SWAA2025072984624.md): Tie Clip · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP LOCATED BS 277, S10R PASSENGER CABIN. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 141A1110, SHEET 18, REV-.
- [SDR SWAA2025072984623](https://openairdocs.org/sdr/SWAA2025072984623.md): Floor Support · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV. REPLACED WEB - INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 14
- [SDR SWAA2025072984622](https://openairdocs.org/sdr/SWAA2025072984622.md): Floor Support · cracked · Jun 23, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02, AND DWG 141A5400, SHE
- [SDR SWAA2025072984484](https://openairdocs.org/sdr/SWAA2025072984484.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Passenger/Crew Doors
  > DETERIORATED LINING ENTRY DOOR NUT ASSIST HANDLE AT FWD GALLEY AREA (4 EA). REPLACED LINING ENTRY DOOR NUT ASSIST HANDLE AT FWD GALLEY AREA (4 EA) IAW AMM 52-11-31-400-802 STEP 3. G. ITEM. (2).
- [SDR SWAA2025072984483](https://openairdocs.org/sdr/SWAA2025072984483.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Passenger/Crew Doors
  > DETERIORATED ENTRY DOORWAY LINING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA). REPLACED ENTRY DOORWAY LINING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA) IAW AMM 25-21-31-420-802 STEP 3.B.(6).
- [SDR SWAA2025072984488](https://openairdocs.org/sdr/SWAA2025072984488.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR LINING ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT AT AFT GALLEY AREA IAW AMM 52-13-31-400-802 STEP 3.G (2).
- [SDR SWAA2025072984491](https://openairdocs.org/sdr/SWAA2025072984491.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED ENTRY DOOR DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA IAW AMM 25-21-25-420-801 STEP 3.B (5).
- [SDR SWAA2025072984489](https://openairdocs.org/sdr/SWAA2025072984489.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Service Doors
  > DETERIORATED SERVICE DOOR LINING ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED SERVICE DOOR LINING ASSIST HANDLE NUT AT AFT GALLEY AREA IAW B737-700 AMM 52-41-31-400-802 STEP 3.F (2).
- [SDR SWAA2025072984490](https://openairdocs.org/sdr/SWAA2025072984490.md): Handle · deteriorated · Jun 22, 2025 · N7887A · Boeing 737752 · Service Doors
  > DETERIORATED SERVICE DOOR DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED SERVICE DOOR DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5).
- [SDR SWAA2025072984478](https://openairdocs.org/sdr/SWAA2025072984478.md): Rib · cracked · Jun 22, 2025 · N7887A · Boeing 737752 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RIB LOCATED LE STA 95.96 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 95.96 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
- [SDR SWAA2025073084042](https://openairdocs.org/sdr/SWAA2025073084042.md): Access Panel · cracked · Jun 21, 2025 · N7887A · Boeing 737752 · Wing, Plate/Skin
  > CRACK ON HOLE ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2025072984040](https://openairdocs.org/sdr/SWAA2025072984040.md): Battery Pack · inoperative · Jun 21, 2025 · N7887A · Boeing 737752 · Emergency Lighting
  > INOP EMERGENCY LIGHT BATTERY PACK BETWEEN BS 727C AND BS 727D LOWER POSITION AT PASSENGER CABIN (1 EA). REPLACED EMERGENCY LIGHT BATTERY PACK BETWEEN BS 727C AND BS 727D LOWER POSITION AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 TESTED OK.
- [SDR SWAA2025072984028](https://openairdocs.org/sdr/SWAA2025072984028.md): Web · cracked · Jun 20, 2025 · N7887A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 55 BETWEEN BS 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.322 IN. APPLIED FILLET-CAP SEALANT LOWER SIDE BETWEEN REPAIR PARTS IAW SOPM 20-50-19 AND INSTALLED FASTENER ON REPAIR ARE
- [SDR SWAA2025072983773](https://openairdocs.org/sdr/SWAA2025072983773.md): Stub Frame · cracked · Jun 20, 2025 · N7887A · Boeing 737752 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S8R TO S9R AT FWD GALLEY DOOR AREA. CRACK LENGTH: 0.937 IN. REPLACED STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY AT PASSENGER CABIN IAW SRM 51-40-02,
- [SDR SWAA2025072884027](https://openairdocs.org/sdr/SWAA2025072884027.md): Pressure Deck · cracked · Jun 20, 2025 · N7887A · Boeing 737752 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.250 IN. INSPECT RII REJECTED STEP 23 DUE TO SEVERAL FASTENER FROM THE INTERNAL SIDE AND EXTERNAL SIDE OF REPAIR WERE FO
- [SDR SWAA2025072983670](https://openairdocs.org/sdr/SWAA2025072983670.md): Skin · corroded · Jun 19, 2025 · N7887A · Boeing 737752 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN VACUUM WASTE VENT CUTOUT LOCATED BTW BS 907 TO BS 927 AND BTW STR 21L TO STR 22L. PERFORMED PERMANENT REPAIR CATEGORY B LOC BTW BS 907 TO BS 927 AND BTW STR 20L TO STR 23L IAW B737-700 SRM 53-70-01-2R-3 AND EA#25-153-01844-WIP1 AND
- [SDR SWAA2025072983659](https://openairdocs.org/sdr/SWAA2025072983659.md): Handle · deteriorated · Jun 19, 2025 · N7887A · Boeing 737752 · Service Doors
  > DETERIORATED SERVICE DOOR CUT OUT ASSISTLE HANDLE NUT AT AFT GALLEY AREA. REPLACED SERVICE DOOR CUT OUT ASSISTLE HANDLE NUT AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801 STEP 3.B (5).
- [SDR SWAA2025072982548](https://openairdocs.org/sdr/SWAA2025072982548.md): Glowstrip · broken · Jun 17, 2025 · N7887A · Boeing 737752 · Emergency Equipment
  > BROKEN PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (5 EA). GENERAL FAULT RESOLVED ON OTHER FAULT TTG8Q00AVU0B.
- [SDR SWAA2025072982558](https://openairdocs.org/sdr/SWAA2025072982558.md): Glowstrip · broken · Jun 17, 2025 · N7887A · Boeing 737752 · Emergency Equipment
  > BROKEN PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN ( 7 EA). GENERAL FAULT RESOLVED ON OTHER FAULT TTG8Q00AVU0B.
- [SDR SWAA2025072982547](https://openairdocs.org/sdr/SWAA2025072982547.md): Door · corroded · Jun 16, 2025 · N7887A · Boeing 737752 · Service Doors
  > CORROSION WASTE SERVICE DOOR 145AL AT FUSELAGE EXTERIOR 2025-388032<[01] TOOL USED ON STEP 4: UT EQUIPMENT P/N: 45MG;S/N:232019809;DUE DATE: 08-OCT-25.<BR>TOOL USED ON STEP 5: EDDY CURRENT EQUIPMENT NORTEC 600D; S/N:240525411; DUE DATE: 13-NOV-25;[02] PERFORME
- [SDR SWAA2025072982546](https://openairdocs.org/sdr/SWAA2025072982546.md): Door · corroded · Jun 16, 2025 · N7887A · Boeing 737752 · Fluid Service Doors
  > CORROSION HINGE WASTE SERVICE DOOR 145AL AT FUSELAGE EXTERIOR. REPLACED HINGE WASTE SERVICE DOOR 145AL AT FUSELAGE EXTERIOR IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7410 SHEET:6 REV -.
- [SDR SWAA2025051268559](https://openairdocs.org/sdr/SWAA2025051268559.md): Light · missing · May 8, 2025 · N7887A · Boeing 737752 · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 24ABC PHOTOLUMINESCENT STRIP MISSING<[01] INSTALLED MISSING STRIP PER AMM 33-51-15;[02] INSPECTION C/W INSTALLED MISSING STRIP PER AMM 33-51-15
- [SDR SWAA2024122668002](https://openairdocs.org/sdr/SWAA2024122668002.md): Fuel Unit · leaking · Dec 21, 2024 · N7887A · Boeing 737752 · Fuel Indicating System
  > POSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE; FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. HOWEVER IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FROM THE LEFT MAIN TANK 12/24
- [SDR SWAA2024122668003](https://openairdocs.org/sdr/SWAA2024122668003.md): Fuel Unit · leaking · Dec 21, 2024 · N7887A · Boeing 737752 · Fuel Indicating System
  > SUPPLEMENTAL INFORMATION: POSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE; FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. HOWEVER IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FRO

Next page: https://openairdocs.org/aircraft/N7887A/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 = 'N7887A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7887A/reports

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