# Service difficulty reports: N7875A

A list on [N7875A](https://openairdocs.org/aircraft/N7875A.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 · 245 reports

- [SDR SWAA2026072131862](https://openairdocs.org/sdr/SWAA2026072131862.md): Cover · damaged · Jul 17, 2026 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > ILLUMINATED LOWER EXIT SIGN AT R/H OVERWING EXIT HAS DAMAGED VERBIAGE. REPLACED LOWER EXIT SIGN COVER AT R/H OVERWING EXIT REF. AMM 33-51-01.
- [SDR SWAA2026060107574](https://openairdocs.org/sdr/SWAA2026060107574.md): Sensor · faulty · May 29, 2026 · N7875A · Boeing 7377Q8 · Trailing Flap Position Indicating System
  > TAKE OFF CONFIG WARNING ON TAKE OFF. FLAPS INDICATION SPLIT RIGHT 1/2 DEGREE HIGHER THEN LEFT. FOUND FC 27-53255 FLAP 6 SKEW. REPLACED 6 FLAP SKEW SENSOR IAW AMM 27-59-01. OPS CHECKED GOOD.
- [SDR SWAA2026060196871](https://openairdocs.org/sdr/SWAA2026060196871.md): Angle · cracked · May 8, 2026 · N7875A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > CRACK ANGLE LOCATED IRSS 139 TRAILING EDGE AT RT WING. REPLACED ANGLE LOCATED IRSS 139 TRAILING EDGE AT RT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0.<
- [SDR SWAA2026060196874](https://openairdocs.org/sdr/SWAA2026060196874.md): Support Beam · cracked · May 8, 2026 · N7875A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > CRACKED SUPPORT BEAM ORSS 297 TRAILING EDGE AT LT WING. REPLACED SUPPORT BEAM LOCATED BTW ORSS 277 TO ORRS 328 APROX. TRAILING EDGE AT LT WING IAW SRM 51-10-02; ITEM 9; SRM 51-40-02 AND DWG 115A3700 SHEET 31; REV-.
- [SDR SWAA2026060196872](https://openairdocs.org/sdr/SWAA2026060196872.md): Plate · damaged · May 8, 2026 · N7875A · Boeing 7377Q8 · Wing Main, Frame Structure
  > ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9.
- [SDR SWAA2026060196873](https://openairdocs.org/sdr/SWAA2026060196873.md): Plate · damaged · May 8, 2026 · N7875A · Boeing 7377Q8 · Wing Main, Frame Structure
  > ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-03-0G-0 AND DWG: 115A2714 SHEET: 11 REV -.
- [SDR SWAA2026060196179](https://openairdocs.org/sdr/SWAA2026060196179.md): Strap · corroded · May 6, 2026 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL156 AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 14
- [SDR SWAA2026060196180](https://openairdocs.org/sdr/SWAA2026060196180.md): Support Bracket · cracked · May 6, 2026 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET BS 867, S3R. REPLACED BRACKET SUPPORT LOCATED BS867 AT LEVEL STR 3R AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 58 REV-.
- [SDR SWAA2026060195684](https://openairdocs.org/sdr/SWAA2026060195684.md): Floor Panel · delaminated · May 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
- [SDR SWAA2026060195686](https://openairdocs.org/sdr/SWAA2026060195686.md): Floor Panel · delaminated · May 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231XF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL. S
- [SDR SWAA2026060195805](https://openairdocs.org/sdr/SWAA2026060195805.md): Window Post · cracked · May 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Main, Structure
  > CRACK WINDOW 1 POST INTERNAL AREA AFT UPPER CORNER POSITION RH SIDE. PERFORMED REPAIR ON UPPER CORNER WINDOW R1 AT COCKPIT AREA IAW EA 26-153-01227 THRU WIP1 TO WIP2.
- [SDR SWAA2026060195177](https://openairdocs.org/sdr/SWAA2026060195177.md): Pressure Blkhd · cracked · May 4, 2026 · N7875A · Boeing 7377Q8 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOCATED BTW RBL 30 TO RBL 60 BTW BS663.75 TO BS675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2026060195306](https://openairdocs.org/sdr/SWAA2026060195306.md): Seat Track · corroded · May 4, 2026 · N7875A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LOCATED BTW BS 500B BS500C WL208 AND LBL 45.50 AT PASSENGER CABIN. REWORKED AND EVALUATED AREA ON SEAT TRACK LOCATED BTW BS 500B TO BS 500C WL208 AND LBL 45.50 AT PASSENGER CABIN-0 PARAGRAPH 9 AND SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1.
- [SDR SWAA2025100822131](https://openairdocs.org/sdr/SWAA2025100822131.md): Light · inoperative · Oct 7, 2025 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT THE CABIN. REMOVED AND REPLACED IAW AMM 33-51-03-960-801.
- [SDR SWAA2025060577660](https://openairdocs.org/sdr/SWAA2025060577660.md): Girt Bar · out of adjust · Jun 2, 2025 · N7875A · Boeing 7377Q8 · Emergency Equipment
  > RH FWD SERVICE DOOR AFT GIRT BAR HOOK IS LOOSE RH FWD SVC DOOR <[01]. C/W EA M-23-125-01839 TEMP REPAIR.
- [SDR SWAA2025012890255](https://openairdocs.org/sdr/SWAA2025012890255.md): Lens · wrong part · Jan 28, 2025 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2024082128481](https://openairdocs.org/sdr/SWAA2024082128481.md): Sign · inoperative · Aug 21, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06 NO FIX. REMOVED AND REPLACED BATTERY C
- [SDR SWAA2024082128709](https://openairdocs.org/sdr/SWAA2024082128709.md): Battery Pack · inoperative · Aug 21, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06 NO FIX. REMOVED AND REPLACED BATTERY C
- [SDR SWAA2024082128711](https://openairdocs.org/sdr/SWAA2024082128711.md): Charger · inoperative · Aug 21, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06 NO FIX. REMOVED AND REPLACED BATTERY C
- [SDR SWAA2024070906947](https://openairdocs.org/sdr/SWAA2024070906947.md): Light · inoperative · Jun 29, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF AMM 33-51-04-960-801. OPERATIONAL TEST PASSED;[02] VERIFIED STEP 1.
- [SDR SWAA2024070906946](https://openairdocs.org/sdr/SWAA2024070906946.md): Light · inoperative · Jun 29, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY OVERHEAD BIN LIGHT AT SEAT ROW 6L/H INOPERATIVE.<[01] RELAMPED EMERGENCY OVERHEAD BIN LIGHT AT SEAT ROW 6L/H AS PER REF AMM 33-51-03-960-801. OPERATIONAL TEST PASSED.;[02] VERIFIED STEP 1.
- [SDR SWAA2024070906467](https://openairdocs.org/sdr/SWAA2024070906467.md): Battery Pack · inoperative · Jun 27, 2024 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > MULTIPLE PAX EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1672 AND M1674 AS PER REF B737 AMM 33-51-06-960-805. OPERATIONAL TEST PASSED.;[02] VERIFIED STEP 1.
- [SDR SWAA2024070902654](https://openairdocs.org/sdr/SWAA2024070902654.md): Floor Panel · deteriorated · Jun 17, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > FOUND PANEL 231UF DETERIORATED. FOUND MAIN CABIN FLOOR PANEL 231UF DETERIORATED.<[01] REPLACED MAIN CABIN FLOOR PANEL 231UF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL 231UF WILL BE INSTALL ON FAULT TTG8Q00TNX25;[02] VERIFIED 1
- [SDR SWAA2024070903520](https://openairdocs.org/sdr/SWAA2024070903520.md): Connector · defective · Jun 14, 2024 · N7875A · Boeing 7377Q8 · Light System Wiring
  > AFT CARGO CONNECTOR D11082 M/W L00547 FOUND DEFECTIVE AT STA 747<[01] REMOVED AND REPLACED AFT CARGO CONNECTOR D11082 M/W L00547 AS PER REF B737 SWPM 20-61-28 AND WDM 33-51-13. PERFORMED EMERGENCY LIGHT - OPERATIONAL CHECK AS PER REF AMM 33-51-00-720-801; TEST
- [SDR SWAA2024070901753](https://openairdocs.org/sdr/SWAA2024070901753.md): Floorbeam · cracked · Jun 14, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > MAIN CABIN FLOOR STRUCTURE PANEL BREAK ASSY STA 540 BL 0 TO LBL 25 FOUND CRACKED<[01] REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT BREAK PANEL ASSY. AT STA 540; FROM BL 0 TO LBL 25 AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
- [SDR SWAA2024070997589](https://openairdocs.org/sdr/SWAA2024070997589.md): Support Fitting · damaged · Jun 2, 2024 · N7875A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > L/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B AFT SUPPORT ROD UPPER SUPPORT FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR SPAR FIXED T/E LOWER PANEL 551GB SUPPORT ROD UPPER SUPPORT FITTING; REF SRM 51-40-02-0G-0;[02] VERIFIED REMOVED AN
- [SDR SWAA2024070997588](https://openairdocs.org/sdr/SWAA2024070997588.md): Fitting · cracked · Jun 2, 2024 · N7875A · Boeing 7377Q8 · Wing, Attach Fittings
  > L/W REARE SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED BULB SEAL FITTING AT L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER AREA; PER B 737-700 SRM 51-40-02-0G-0 AND BOEING DW
- [SDR SWAA2024070991681](https://openairdocs.org/sdr/SWAA2024070991681.md): Attach Fitting · corroded · May 30, 2024 · N7875A · Boeing 7377Q8 · Emergency Equipment
  > FLIGHT COMPARTMENT LH ESCAPE ROPE WORN SPOTS AND ATTACH FITTING WITH CORROSION.<[01] REMOVED AND REPLACED LH ESCAPE ROPE AS REF. B737-700 AMM 25-61-10-000-801 AND AMM 25-61-10-400-801.;[02] VERIFIED ESCAPE ROPE REPLACEMENT.<BR>AUDIT CW PER MPM 52.02.02.
- [SDR SWAA2024070991682](https://openairdocs.org/sdr/SWAA2024070991682.md): Escape Rope · worn · May 30, 2024 · N7875A · Boeing 7377Q8 · Emergency Equipment
  > FLIGHT COMPARTMENT RH ESCAPE ROPE WORN SPOTS AND ATTACH FITTING WITH CORROSION.<[01] REMOVED AND REPLACED RH ESCAPE ROPE AS REF. B737-700 AMM 25-61-10-000-801 AND AMM 25-61-10-400-801.;[02] VERIFIED REPLACEMENT OF ESCAPE ROPE/LANYARD.<BR>AUDIT CW PER MPM 52.02
- [SDR SWAA2024070991297](https://openairdocs.org/sdr/SWAA2024070991297.md): Floor Panel · corroded · May 29, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT;CAP STRIP FLOOR PANEL 140DF HAS CORROSION.<[01] RECIEVED NEW AFT CARGO COMP CAP STRIP FLOOR PANEL 140DF P/N 453A2611-5 INSTALLATION WILL BE ACCOMPLISHED ON JOB CARD TTG8Q00SRQLV PER REF AMM 25-52-10-400-801.;[02] VERIFIED STEP1<BR>AUDIT P
- [SDR SWAA2024070990626](https://openairdocs.org/sdr/SWAA2024070990626.md): Floor Panel · delaminated · May 28, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL # 232SF COMPOSITE MATERIAL DELAMINATION AT AFT INB CORNER.<[01] REPAIRED DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL #232SF AS PER B737 SRM 53-00-50-2R-9. MATERIAL USED PO#2039827 AND PO#1738579.;[02] REPAIRED DAMAGE AREA AS MARKED O
- [SDR SWAA2024070990625](https://openairdocs.org/sdr/SWAA2024070990625.md): Floor Panel · peeling · May 28, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL # 231XF COMPOSITE MATERIAL PEELING OFF.<[01] RECEIVED NEW CABIN FLOOR PANEL #231XF P/N 144A5810-126; REFERENCE AAR TAG # PD232; PO# 2059779. FLOOR PANEL INSTALLATION WILL OCCUR ON TASK CARD: TTG8Q00SRNYW.;[02] VERIFIED STEP 1<BR><BR>AUDI
- [SDR SWAA2024070990624](https://openairdocs.org/sdr/SWAA2024070990624.md): Floor Panel · delaminated · May 28, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL # 241BF COMPOSITE MATERIAL DELAMINATION AT FWD INB CORNER.<[01] RECEIVED NEW CABIN FLOOR PANEL #241BF P/N 144A5810-189; REFERENCE AAR TAG # PD229; PO# 2059779. FLOOR PANEL INSTALLATION WILL OCCUR ON TASK CARD: TTG8Q00SRNWA.;[02] VERIFIED
- [SDR SWAA2024070990617](https://openairdocs.org/sdr/SWAA2024070990617.md): Floor Panel · peeling · May 28, 2024 · N7875A · Boeing 7377Q8 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL # 241FF COMPOSITE MATERIAL PEELING OFF.<[01] RECEIVED NEW CABIN FLOOR PANEL #241FF P/N 144A5810-131; REFERENCE AAR TAG # HA1091; PO# 2059779. FLOOR PANEL INSTALLATION WILL OCCUR ON TASK CARD: TTG8Q00SRNW2;[02] VERIFIED STEP 1<BR><BR>AUDI
- [SDR SWAA2024070989994](https://openairdocs.org/sdr/SWAA2024070989994.md): Panel · cracked · May 25, 2024 · N7875A · Boeing 7377Q8 · Passenger/Crew Doors
  > AFT ENTRY DOOR (L-2) PANEL 834DZ IS CRACKED AND BENT ALL AROUND. (DOT #28-1)<[01] REPLACED AFT ENTRY DOOR (L-2) PANEL 834DZ PER SRM 51-40-02-0G-0;[02] CORRECTION TO STEP 1: REPLACED AFT ENTRY DOOR (L-2) PANEL 834DZ PER SRM 51-40-02-0G-0. INSTALLATION OF AFT EN
- [SDR SWAA2024070989655](https://openairdocs.org/sdr/SWAA2024070989655.md): Seat Track · corroded · May 24, 2024 · N7875A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CROWN BOTTOM AREA HAS CORROSION SPOTS BETWEEN STA 360+11' TO 380 LBL 45.50 MKD (107-023)<[01] REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 360+10 TO STA 480; LBL 45.5 AS PER SRM 51-40-02-0G-0 AND DWG 143A5300;[02] VERIFIED REMOVED AND REPLAC
- [SDR SWAA2024070989645](https://openairdocs.org/sdr/SWAA2024070989645.md): Seat Track · chafed · May 24, 2024 · N7875A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARK AT STA 520 LBL 24.75 MKD (107-016) MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARKS AND GOUGE AT STA 520 LBL 24.75<[01] ACCOMPLISHED PERMANENT REPAIR CATEGORY 'A' AT SECTION 43 SEAT TRACK LBL 24.7
- [SDR SWAA2024070989648](https://openairdocs.org/sdr/SWAA2024070989648.md): Seat Track · chafed · May 24, 2024 · N7875A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARK AT STA 520 LBL 45.50 MKD (107-017)<[01] EVALUATED DAMAGE REMOVAL AT SEAT TRACK CROWN UPPER SURFACE; MATERIAL REMOVED 0.026' MAXIMUM ALLOWABLE REMOVAL 0.020'. FOUND OUT OF LIMITS REF SRM 53-00-52-1A-1<BR>D
- [SDR SWAA2024070989552](https://openairdocs.org/sdr/SWAA2024070989552.md): Doubler · cracked · May 24, 2024 · N7875A · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER RECEPTACLE ACCESS DOOR CUTOUT SKIN DOUBLER HAS A CRACK AT LOWER SIDE (AT FASTENER)<[01] REMOVED AND DISCARDED DAMAGED EGPR DOUBLER; LOCATED; DRILLED AND INSTALLED NEW EXTERNAL GROUND POWER RECEPTACLE DOUBLER AS PER B737-700 SRM 51-40-02-0G-0 AND
- [SDR SWAA2024070989649](https://openairdocs.org/sdr/SWAA2024070989649.md): Seat Track · corroded · May 24, 2024 · N7875A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CROWN BOTTOM AREA HAS CORROSION SPOTS BETWEEN STA 360+11' TO 380 LBL 24.75 MKD (107-024)<[01] REMOVED AND REPLACED SEAT TRACK FROM STA 360+ 10 TO STA 480 LBL 24.75; REF SRM 51-40-02-0G-0 AND DWG# 143A5300;[02] VERIFIED REMOVED AND REPLACED SEA
- [SDR SWAA2024070989135](https://openairdocs.org/sdr/SWAA2024070989135.md): Scuff Plate · deteriorated · May 23, 2024 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > ANTI-SKID TAPE AT MAIN ENTRY AND SERVICE DOORS L-1; L-2; R-1 AND R-2 SCUFF PLATES DETERIORATED<[01] INSTALLED ANTI-SKID TAPE AT MAIN ENTRY AND SERVICE DOORS L-1; L-2; R-1 AND R-2 SCUFF AS PER REFE AMM 53-11-01-420-801.;[02] VERIFIED NON-SKID TAPE INSTALLATION.
- [SDR SWAA2023090697211](https://openairdocs.org/sdr/SWAA2023090697211.md): Light · out of adjust · Sep 6, 2023 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > ROW 1DEF CENTER ISLE PHOTOLUMINESCENT STRIP HAS MOISTURE IN IT AND LOOSE.<[01] REMOVED AND REPLACED 1DEF PHOTOLUMINESCENT STRIIP IAW AMM 33-51-15.
- [SDR SWAA2023042630505](https://openairdocs.org/sdr/SWAA2023042630505.md): Light · inoperative · Apr 23, 2023 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON RIGHT HAND OVERWING EXIT INOP<[01] RE-LAMPED EMERGENCY EXIT INFORMATION LIGHT ON RIGHT HAND OVERWING EXIT IN REF TO AMM 33-25-00. OPS TEST GOOD
- [SDR SWAA2022091952989](https://openairdocs.org/sdr/SWAA2022091952989.md): None · faulty · Sep 14, 2022 · N7875A · Boeing 7377Q8 · Trailing Edge Flap Control System
  > ON APPROACH FLAP HANDLE PLACED TO 1. LEFT TRAILING EDGE FLAP INDICATOR SHOWED LESS THAN 1. RT TRAILING EDGE FLAP INDICATOR SHOWED 0. NO LEADING EDGE FLAP MOVEMENT OR LIGHTS. LANDED AT 167 KIAS. AUTO BRAKES MAX USED. BRAKING COOLING MODULE SAYS 31.9M FT-LB. COO
- [SDR SWAA2022081040438](https://openairdocs.org/sdr/SWAA2022081040438.md): Hook · broken · Aug 10, 2022 · N7875A · Boeing 7377Q8 · Emergency Equipment
  > AFT ENTRY DOOR GIRT BAR PLASTIC CLIP BROKEN / [01] REMOVED AND REPLACED GIRT BAR STOP RING PER AMM 25-66-01.
- [SDR SWAA2022060814418](https://openairdocs.org/sdr/SWAA2022060814418.md): Battery Pack · inoperative · Jun 2, 2022 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY LIGHTS COMMON TO BATTERY PACK M1668 ARE INOP. / [01] REPLACED; AND PERFORMED GOOD TEST OF BATTERY PACK M1668 PER AMM 33-51-06-960-805.;[02] VERIFIED ALL ITEMS COMPLETE.;[03] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2022060814417](https://openairdocs.org/sdr/SWAA2022060814417.md): Light · inoperative · Jun 2, 2022 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > AFT ENTRY DOOR SLIDE LIGHT INOP. / [01] REPLACED LAMP AND PERFORMED GOOD TEST OF AFT ENTRY DOOR SLIDE LIGHT PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2022060813419](https://openairdocs.org/sdr/SWAA2022060813419.md): Light · inoperative · May 30, 2022 · N7875A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COME ON WHEN POWER IS OFF AND SWITCH IS ALSO OFF / [01] WHILE TROUBLESHOOTING DISCOVERED W4142-0032-22 WAS BROKEN CAUSING THE EMERG. EXIT LIGHTS TO COME ON WHEN POWER WAS OFF THE AIRCRAFT AND THE SWITCH WAS OFF. SPLICED WIRE W4142-0032-22
- [SDR SWAA2022060808279](https://openairdocs.org/sdr/SWAA2022060808279.md): Intercostal · cracked · May 17, 2022 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL AT AFT CARGO BAY BS 927-BS 947 RBL 21 / [01] DAMAGE FOUND ON AFT CARGO BAY INTERCOSTAL BS 927- BS947 RBL 21 FOUND TO BE OUT OF LIMIT PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9C;[02] RECIVED NEW INTERCOSTAL ITEM 147A75
- [SDR SWAA2022060807253](https://openairdocs.org/sdr/SWAA2022060807253.md): Angle · cracked · May 12, 2022 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK IN VERTICAL L ANGLE BS 692 RBL 0.5 WL 206.5. VERIFIED THE APPLICABILITY OF SRM 51-10-02-0G-0; REMOVED THE CRACKED VERTICAL L ANGLE BS 692 RBL 0.5 WL 206.5 DUE TO NO ALLOWABLE LIMITS FOR CRACKS IAW SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0;FORMED NEW VERTIC

Next page: https://openairdocs.org/aircraft/N7875A/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 = 'N7875A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7875A/reports

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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.