# Service difficulty reports: N7888A

A list on [N7888A](https://openairdocs.org/aircraft/N7888A.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 · 242 reports

- [SDR SWAA2026102612487](https://openairdocs.org/sdr/SWAA2026102612487.md): Hook · loose · Oct 20, 2026 · N7888A · Boeing 737752 · Emergency Equipment
  > FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR HOOKS LOOSE. ADJUSTED & TIGHTENED THE GIRT BAR HOOKS IAW AMM 52-41-00.
- [SDR SWAA2026101574936](https://openairdocs.org/sdr/SWAA2026101574936.md): Manifold · leaking · Oct 11, 2026 · N7888A · Boeing 737752 · Air Distribution System
  > CARGO FIRE EXTINGUISHING, DISCHARGE LIGHT ON, DISCHARGE SWITCH NOT PUSHED. FOUND AIR CONDITIONING DUCT LEAK BLOWING COLD AIR NEAR CARGO FIRE BOTTLES. REMOVED AND REPLACED MIX MANIFOLD IAW AMM 21-21-05-400-801. NO LEAKS NOTED. CARGO DISCHARGE LIGHT EXTINGUISH
- [SDR SWAA2026083137585](https://openairdocs.org/sdr/SWAA2026083137585.md): Seal · cracked · Aug 26, 2026 · N7888A · Boeing 737752 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED ALONG SEAL TRACK EDGE. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. REF AMM 53-31-31.
- [SDR SWAA2026083157366](https://openairdocs.org/sdr/SWAA2026083157366.md): Paint · missing · Aug 26, 2026 · N7888A · Boeing 737752 · Spoilers
  > RIGHT WING #7 GROUND SPOILER UPPER SURFACE MISSING WING WALK PAINT AND EMERGENCY EGRESS ARROW APPLIED OVERWING EMERGENCY WALKWAY PAINT (WHITE) ON RIGHT WING #7 SPOILER PER AMM 51-21-97. EMERGENCY EGRESS ARROWS APPLICATION REQUIRED APPLIED EMERGENCY EGRESS ARRO
- [SDR SWAA2025120842643](https://openairdocs.org/sdr/SWAA2025120842643.md): Lamp · inoperative · Dec 4, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > L-1 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. REPLACED THE LAMPS AND PERFORMED GOOD OPS CHECK OF L1 EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-04-960-801.
- [SDR SWAA2025120842249](https://openairdocs.org/sdr/SWAA2025120842249.md): Girt Bar · loose · Dec 3, 2025 · N7888A · Boeing 737752 · Emergency Equipment
  > LOOSE FED ESCAPE SLIDE AFT GIRT BAR FITTING. TIGHTENED LOOSE FED ESCAPE SLIDE AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801.
- [SDR SWAA2025120842246](https://openairdocs.org/sdr/SWAA2025120842246.md): Light · debonded · Dec 3, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > DEBONDED EMERGENCY LIGHT PANEL AT OVERHEAD BIN 6, 9, & 11ABC AND 6, 8, & 11DEF. REBONDED CLIPS AT EMERGENCY LIGHT PANEL AT OVERHEAD BIN 6, 9, & 11ABC, AND 6, 8, & 11DEF IAW DWG 412A1607-9B, REV C, 412A1607 REV T. BACS5010, PAGE 64. APPLIED TYPE 70.
- [SDR SWAA2025120841318](https://openairdocs.org/sdr/SWAA2025120841318.md): Support · cracked · Dec 1, 2025 · N7888A · Boeing 737752 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON AFT FAIRING, AFT WEDGE CRACKED AT T/E SUPPORT. EVALUATED DAMAGED AFT WEDGE ASSEMBLY AND FOUND COMPONENT UNSERVICEABLE IAW SRM 54-50-90-1A-1. REMOVED AND REPLACED NR 1 ENGINE PYLON AFT WEDGE ASSY IAW SRM 51-40-02-0G-0, AND DWG 313A2752, SHEET 0
- [SDR SWAA2025120841440](https://openairdocs.org/sdr/SWAA2025120841440.md): Fitting · loose · Dec 1, 2025 · N7888A · Boeing 737752 · Emergency Equipment
  > DURING OK TO CLOSE FWD ENTRY DOOR FOUND ESCAPE SLIDE GIRT BAR FITTING LOOSE. TIGHTENED FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR FITTING IAW AMM 25-66-02-400-801.
- [SDR SWAA2025120841438](https://openairdocs.org/sdr/SWAA2025120841438.md): Fitting · loose · Dec 1, 2025 · N7888A · Boeing 737752 · Emergency Equipment
  > DURING OK TO CLOSE AFT GALLEY DOOR FOUND SCAPE SLIDE GIRT BAR FITTING LOOSE. TIGHTENED AFT GALLEY DOOR ESCAPE SLIDE GIRT BAR FITTING IAW AMM 25-66-02-400-801.
- [SDR SWAA2025120841439](https://openairdocs.org/sdr/SWAA2025120841439.md): Fitting · loose · Dec 1, 2025 · N7888A · Boeing 737752 · Emergency Equipment
  > DURING OK TO CLOSE, AFT ENTRY DOOR FOUND ESCAPE SLIDE GIRT BAR FITTING LOOSE. TIGHTENED AFT ENTRY DOOR ESCAPE SLIDE GIRT BAR FITTING IAW AMM 25-66-02-400-801.
- [SDR SWAA2025120839725](https://openairdocs.org/sdr/SWAA2025120839725.md): Attach Bracket · corroded · Nov 26, 2025 · N7888A · Boeing 737752 · Fuselage Main, Attach Fittings
  > CORROSION ON NOSE RADOME ATTACH BRACKET AT BS 178; RBL 12; WL 240.1. REMOVED AND REPLACED CLIP IAW AMM 53-52-00-400-801.
- [SDR SWAA2025120836545](https://openairdocs.org/sdr/SWAA2025120836545.md): Wire · detached · Nov 19, 2025 · N7888A · Boeing 737752 · Light System Wiring
  > FWD ENTRY DOOR BS 303, S17L WIRE NOT PINNED TO GROUND BLOCK. REPAIRED THE WIRE W4142-0152-20 AND TERMINATED ON GD3752 IAW WDM 33-51-21 AND SWPM 20-90-15.
- [SDR SWAA2025120836544](https://openairdocs.org/sdr/SWAA2025120836544.md): Floor Panel · cracked · Nov 18, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > WHILE CLOSING-ZONE 120 FCB, NOTED SEVERAL CRACKS ON EDGE AND DAMAGE ON FLOOR PANEL 120BF. FABRICATED A NEW FCB FLOOR PANEL 120BF IAW AMM 25-52-01-201-801.
- [SDR SWAA2025120836437](https://openairdocs.org/sdr/SWAA2025120836437.md): Splice · corroded · Nov 18, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FLOOR PANEL SPLICE AT BS 727D+7 HAS CORROSION. NO ALLOWABLE DAMAGE FOUND FOR FLOR PANEL SPLICE. REMOVED AND REPLACED THE SPLICE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025120834885](https://openairdocs.org/sdr/SWAA2025120834885.md): Stand Off · debonded · Nov 13, 2025 · N7888A · Boeing 737752 · Fuselage Main, Attach Fittings
  > CEILING PANEL 241YAC EXIT SIGN WIRE STANDOFF IS DIBONDED. BONDED THE EXIT WIRE STANDOFF IAW AMM 20-30-11-910-801.
- [SDR SWAA2025120834884](https://openairdocs.org/sdr/SWAA2025120834884.md): Support · cracked · Nov 13, 2025 · N7888A · Boeing 737752 · Passenger/Crew Doors
  > LOWER LINER SUPPORT PANEL 841DZ SUPPORT IS CRACKED.<[01] REMOVED AND REPLACED BRACKET AT LOWER LINER SUPPORT 841DZ PER SRM 51-40-02-0G-0 AND BOEING DWG 411A2119 REV -.
- [SDR SWAA2025120834091](https://openairdocs.org/sdr/SWAA2025120834091.md): Light · cracked · Nov 12, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > FOUND NUMEROUS CRACKS ON PHOTOLUMINESCENT STRIP. COMPLETED ALL PHOTOLUMINESCENT STRIP REPLACEMENT FROM BS 420 - 887 MISSING SOME PIECES BECAUSE THE LAVATORY IS NOT INSTALLED. ] REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS IAW DWG 33500007, & AMM 33-51-15-40
- [SDR SWAA2025120834506](https://openairdocs.org/sdr/SWAA2025120834506.md): Bracket · cracked · Nov 12, 2025 · N7888A · Boeing 737752 · Wing Miscellaneous Structure
  > RIGHT WING T/E PANEL 651FB FWD EDGE 3RD BRACKET FROM OTBD END CRACKED. REMOVED BROKEN BRACKET & PREP TO INSTALL A NEW BRACKET PER SRM 51-40-02-0G -0. REMOVED AND REPLACED THE RT T/E PANEL 651FB FWD EDGE 3RD BRACKET FROM OTBD END IAW SRM 51-40-02-0G-0. STEP
- [SDR SWAA2025120833689](https://openairdocs.org/sdr/SWAA2025120833689.md): Angle · corroded · Nov 11, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON ACB SHIELD ANGLE, BS 767 - 787, RBL 20, WL 155. FOUND FAULT DURING REMOVAL OF SHIELD. REMOVED AND REPLACED ACB SHIELD ANGLE IAW SRM 51-40-02, AND DWG 146A0081, REV- AND DWG 146A8123, REV-.
- [SDR SWAA2025120834008](https://openairdocs.org/sdr/SWAA2025120834008.md): Baffle · cracked · Nov 11, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE AT BS 500A - 500B, RBL 21, WL 156 IS CRACKED. REMOVED, REPAIRED, AND INSTALLED A NEW BAFFLE ASSY IAW SRM 51-40-02, DWG 143A7505, REV A, AND SRM 53-30-53-2R-1-A01785, REPAIR 1 - SECTION 43.
- [SDR SWAA2025120834090](https://openairdocs.org/sdr/SWAA2025120834090.md): Baffle · corroded · Nov 11, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT ACB BAFFLE BS 747 - 767, APPOX RBL 21, WL 155. CORROSION ON BAFFLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED, & REPLACED THE BAFFLE IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A7502 REV -.
- [SDR SWAA2025120834085](https://openairdocs.org/sdr/SWAA2025120834085.md): Rib · cracked · Nov 11, 2025 · N7888A · Boeing 737752 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB REMOVABLE L/E INBD END RIB IS CRACKED. REMOVED CRACKED RIB FROM RT STAB L/E IAW SRM 51-40-02-0G-0 & INSTALLED IAW DWG 186A1001 REV B, SRM 51-40-02-0G-0, & SRM 55-10-01-2R-1.
- [SDR SWAA2025120833685](https://openairdocs.org/sdr/SWAA2025120833685.md): Sidewall Support · corroded · Nov 10, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A - 500D, RBL 22, WL 156. FLOOR TO SIDEWALL SUPPORT REPLACED ON WORK CARD TTG8Q018T0R0.
- [SDR SWAA2025120833686](https://openairdocs.org/sdr/SWAA2025120833686.md): Shield · corroded · Nov 10, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY FLOOR AFT SHIELD DOOR CUTOUT AT BS 492 500A, RBL 22, WL 156. REMOVED THE DAMAGED SHIELD IAW SRM 51-40-02. & INSTALLED A NEW SHIELD IAW SRM 51-40-02 AND DWG 143A0080 REV-.
- [SDR SWAA2025120833407](https://openairdocs.org/sdr/SWAA2025120833407.md): Sidewall Support · corroded · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727B - 847, LBL 21, WL 155. FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED A NEW FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 847, & SPLICE AT BS 727E+9.8, LBL 21, WL 155 IAW SRM 53-00-53-1A
- [SDR SWAA2025120833412](https://openairdocs.org/sdr/SWAA2025120833412.md): Support · corroded · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SHEILD SUPPORT AT BS 847 - 867, RBL 24, WL 155. REMOVED AND REPLACED AFT CARGO BAY SHEILD SUPPORT IAW SRM 50-40-02 & DWG 1460081.
- [SDR SWAA2025120833411](https://openairdocs.org/sdr/SWAA2025120833411.md): Support · corroded · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SHEILD SUPPORT AT BS 767 - 794, RBL 24, WL 155. REMOVED AND REPLACED THE SHIELD SUPPORT IAW DWG 146A0081, REV A, AND SRM 51-40-02.
- [SDR SWAA2025120833409](https://openairdocs.org/sdr/SWAA2025120833409.md): Sidewall Support · corroded · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727B - 767, RBL 21, WL 155. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 53-00-53-1A-2, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-20
- [SDR SWAA2025120833176](https://openairdocs.org/sdr/SWAA2025120833176.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232QF HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232QF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9 A.1, DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025120833173](https://openairdocs.org/sdr/SWAA2025120833173.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232JF HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE, REPLACED FLOOR PANEL 232JF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-00-09A, ITEM 61.
- [SDR SWAA2025120833172](https://openairdocs.org/sdr/SWAA2025120833172.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232FF HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232FF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025120833171](https://openairdocs.org/sdr/SWAA2025120833171.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232DF HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232DF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025120833170](https://openairdocs.org/sdr/SWAA2025120833170.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231WF HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231WF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025120833175](https://openairdocs.org/sdr/SWAA2025120833175.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231MF HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231MF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025120833169](https://openairdocs.org/sdr/SWAA2025120833169.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231JF HAS AREAS OF PULLED STRANDS. THE CABIN FLOOR PANEL 231JF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025120833168](https://openairdocs.org/sdr/SWAA2025120833168.md): Floor Panel · pulled · Nov 9, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231FF HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE, REPLACED THE FLOOR PANEL 231FF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-00-09A, ITEM 250.
- [SDR SWAA2025120832525](https://openairdocs.org/sdr/SWAA2025120832525.md): Floor Panel · pulled · Nov 7, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241VF IAW SRM 53-00-50-2R-0 PARA. 1.A NOTE AND DWG 146A5810 0100.
- [SDR SWAA2025120832526](https://openairdocs.org/sdr/SWAA2025120832526.md): Floor Panel · pulled · Nov 7, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241WF IAW SRM 53-00-50-2R-0 PARA. 1.A AND DWG 146A5810 0028.
- [SDR SWAA2025120832527](https://openairdocs.org/sdr/SWAA2025120832527.md): Floor Panel · pulled · Nov 7, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241XF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025120832530](https://openairdocs.org/sdr/SWAA2025120832530.md): Floor Panel · pulled · Nov 7, 2025 · N7888A · Boeing 737752 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 242QF IAW SRM 53-00-50-2R-0 PARA. 1.A NOTE AND DWG 146A5810 ID: 0026.
- [SDR SWAA2025120832821](https://openairdocs.org/sdr/SWAA2025120832821.md): Skin · cracked · Nov 7, 2025 · N7888A · Boeing 737752 · Fuselage Main, Plate/Skin
  > CRACK FOUND AT FED SURROUND STRUCTURE BS 291.5+4, STR 16L. REMOVED AND REPLACED FED SURROUND STRUCTURE BS 291.5+4 S16L, IAW SRM 51-40-02-0G-0 AND DWG 141A8180 REV C.
- [SDR SWAA2025120832820](https://openairdocs.org/sdr/SWAA2025120832820.md): Shield · cracked · Nov 7, 2025 · N7888A · Boeing 737752 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE INBD FAN COWL OIL DOOR SHIELD HAS A CRACK IN IT. REMOVED AND REPLACED THE CRACKED NR 1 ENGINE INBD FAN COWL OIL DOOR SHIELD IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025120831676](https://openairdocs.org/sdr/SWAA2025120831676.md): Scuff Plate · cracked · Nov 5, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FCB FWD CORNER SCUFF PLATE CRACKED. REMOVED FCB FWD CORNER SCUFF PLATE IAW AMM 53-11-02-020-801-NG, REPAIR COMPLETED IAW SRM 53-30-15-2R-1-A00990, REPAIR 1. SCUFF PLATE INSTALLED ON TASK TTG8Q0188ZGC.
- [SDR SWAA2025120831675](https://openairdocs.org/sdr/SWAA2025120831675.md): Scuff Plate · cracked · Nov 5, 2025 · N7888A · Boeing 737752 · Fuselage Miscellaneous Structure
  > FCB AFT CORNER SCUFF PLATE IS CRACKED. REMOVED FCB AFT CORNER SCUFF PLATE IAW AMM 53-11-02-020-801-NG, REPAIR COMPLETED IAW SRM 53-30-15-2R-1-A00990, REPAIR 1. SCUFF PLATE INSTALLED ON TASK TTG8Q0188ZGC.
- [SDR SWAA2025120831080](https://openairdocs.org/sdr/SWAA2025120831080.md): Battery Pack · no test · Nov 3, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > BATTERY PACK M2335 FAILS CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK M2335 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805. PERFORMED GOOD BATTERY PACK CAPACITY CHECK IAW AMM 33-51-06-200-801.
- [SDR SWAA2025120831079](https://openairdocs.org/sdr/SWAA2025120831079.md): Light · inoperative · Nov 3, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > AFT ENTRY DOOR SLIDE LIGHT IS INOPERATIVE. RELAMPED AFT ESCAPE SLIDE LIGHT, L732 AND PERFORMED GOOD LIGHT TEST IAW AMM 33-51-04-960-801.
- [SDR SWAA2025021997637](https://openairdocs.org/sdr/SWAA2025021997637.md): Lamp · inoperative · Feb 19, 2025 · N7888A · Boeing 737752 · Emergency Lighting
  > RH EXTERIOR EMERGENCY LIGHT FWD OF AFT CARGO INOP<[01] RELAMPED PER AMM 33-51-03. OPS CHK GOOD
- [SDR SWAA2024110154485](https://openairdocs.org/sdr/SWAA2024110154485.md): Skin · delaminated · Oct 29, 2024 · N7888A · Boeing 737752 · Trailing Edge Flaps
  > LH OUTBOARD AFT FLAP (P/N 113A3700-19; S/N 000992) UPPER SKIN DELAMINATION AT INBOARD EDGE - PERMANENT REPAIR) [TTG8Q00WPEME]<[01] REMOVED AND REPLACED L/H OUTBOARD AFT FLAP PER AMM 21-51-22. CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME. PARTS AND TOOLS ON (TTG
- [SDR SWAA2024102953911](https://openairdocs.org/sdr/SWAA2024102953911.md): Skin · delaminated · Oct 26, 2024 · N7888A · Boeing 737752 · Trailing Edge Flaps
  > LEFT HAND AFT TRAILING EDGE FLAP HAS EVIDENCE OF DELAMINATION TSR # 20244007602<[01] C/W EA 24-157-02971<BR>OKAY FOR CONT SERVICE

Next page: https://openairdocs.org/aircraft/N7888A/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 = 'N7888A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7888A/reports

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