# Service difficulty reports: N7862A

A list on [N7862A](https://openairdocs.org/aircraft/N7862A.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 · 236 reports

- [SDR SWAA2025110531910](https://openairdocs.org/sdr/SWAA2025110531910.md): Coalescer Bag · odor · Nov 4, 2025 · N7862A · Boeing 73779P · Humidity Control System
  > ON TAXI IN, STARTED APU, TURNED ON APU AIR. SMELLED SMOKE, TURNED OFF APU AIR AND APU. TURNED OFF RECIRCULATION FAN ODOR CLEARED. SMOKE ODOR IN ENTIRE CABIN, FWD AND AFT. C/W INSPECTION 05-51-56-0200-801 COULD NOT DUPLICATE. REPLACED COALESCER BAGS NR 1 &
- [SDR SWAA2025110327051](https://openairdocs.org/sdr/SWAA2025110327051.md): Lamp · not seated · Oct 22, 2025 · N7862A · Boeing 73779P · Emergency Lighting
  > LEFT EMERGENCY EXIT HATCH OVERHEAD LIGHT INOPERATIVE. ON INVESTIGATION FOUND LT EMERGENCY EXIT HATCH OVERHEAD LAMP INCORRECTLY SEATED, SEATED CORRECTLY AND PERFORMED GOOD LAMP TEST IAW AMM 33-21-00-960-801.
- [SDR SWAA2025110327053](https://openairdocs.org/sdr/SWAA2025110327053.md): Connector · disconnected · Oct 22, 2025 · N7862A · Boeing 73779P · Light System Wiring
  > SEVERAL RT & LT OVERHEAD STOWAGE BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED CONNECTOR D13018 TO EMERGENCY LIGHT POWER SUPPLY M2335 IAW AMM 33-51-06-960-806 AND PERFORMED SATISFACTORY OPS TEST IAW AMM 33-51-00-710-801.
- [SDR SWAA2025110323750](https://openairdocs.org/sdr/SWAA2025110323750.md): Glowstrip · damaged · Oct 12, 2025 · N7862A · Boeing 73779P · Emergency Equipment
  > MULTIPLE PHOTOLUMINESCENT STRIPS FOUND DAMAGED. REPLACED AND INSTALLED NEW PHOTOLUMINESCENTS STRIPS KIT IAW DWG 33500007, REV 2.
- [SDR SWAA2025103022363](https://openairdocs.org/sdr/SWAA2025103022363.md): Rib · cracked · Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 1 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-4.
- [SDR SWAA2025103022364](https://openairdocs.org/sdr/SWAA2025103022364.md): Rib · cracked · Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 4 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-5.
- [SDR SWAA2025103022362](https://openairdocs.org/sdr/SWAA2025103022362.md): Rib · cracked · Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACKS LOCATED AT RT HORIZONTAL STAB NR 4 RIB HSS 120.30, FRONT SPAR ATTACH STIFFENER. REMOVED AND REPLACED RT HORIZONTAL STAB RIB FRONT STIFFENER IAW SRM 51-40-02-0G-0 AND DWG 142A2401 REV:F.
- [SDR SWAA2025110421441](https://openairdocs.org/sdr/SWAA2025110421441.md): Angle · deformed · Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > DEFORMED ANGLE RBL20.6 STA1096 WL 249.61 HORIZONTAL BEAM LOWER. RII ITEMS COMPLIED WITH ON 25-153-02689-WIP1-WIP4. NO RII REQUIREMENTS ON 25-153-01768-WIP1. REMOVED AND REPLACE ANGLE IAW EA 25-153-02689.
- [SDR SWAA2025110421439](https://openairdocs.org/sdr/SWAA2025110421439.md): Stiffener · deformed · Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > DEFORMED STIFFENER BS 1096, RBL 10 - 30.6, WL 249.61 HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02-0G-0 AND EA 25-153-02689, FIGURE 3, SHEET 1.
- [SDR SWAA2025110321440](https://openairdocs.org/sdr/SWAA2025110321440.md): Stiffener · deformed · Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > DEFORMED STIFFENER BS 1088, RBL 15 TO RBL 29, WL 249.61. HORIZONTAL BEAM LOWER. REFER TO FAULT TTG8Q015D0QP WHERE EA 25-153-02689 WAS ADDED AS A SUBTASK..
- [SDR SWAA2025110321438](https://openairdocs.org/sdr/SWAA2025110321438.md): Angle · deformed · Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > DEFORMED ANGLE, RBL 20.6, BS 1088 - 1096, WL 249.61, HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND EA 25-153-02689, FIGURE 3, SHEET 1.
- [SDR SWAA2025103018362](https://openairdocs.org/sdr/SWAA2025103018362.md): Intercostal · corroded · Sep 26, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 TO 787 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G, AND DWG 146A8130, REV B.
- [SDR SWAA2025103018363](https://openairdocs.org/sdr/SWAA2025103018363.md): Intercostal · corroded · Sep 26, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 787 TO 807 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G AND DWG 146A8130, REV B.
- [SDR SWAA2025110318359](https://openairdocs.org/sdr/SWAA2025110318359.md): Web · corroded · Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SUB WEB THRESHOLD AT BS 794 - 847, RBL 25, WL 155. REMOVED AND REPLACED ACB SUB THRESOLD WEB IAW SRM 51-40-02 AND DWG 146A8120 REV: E.
- [SDR SWAA2025103018360](https://openairdocs.org/sdr/SWAA2025103018360.md): Intercostal · corroded · Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 - 807, RBL 6, WL 150. OPEN
- [SDR SWAA2025103018356](https://openairdocs.org/sdr/SWAA2025103018356.md): Sidewall Support · corroded · Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, LBL 21, WL 155. REMOVED & REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 & DWG 146A7500, REV B.
- [SDR SWAA2025103018361](https://openairdocs.org/sdr/SWAA2025103018361.md): Sidewall Support · corroded · Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, RBL 21, WL155. REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, & DWG 146A7500 ID: 0085 REV A.
- [SDR SWAA2025110417169](https://openairdocs.org/sdr/SWAA2025110417169.md): Seat Track · corroded · Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK, LBL 45, BS 480+18, 500A+9, 500D+10. THIS FAULT WILL BE RESOLVED IN FAULT TTG8Q015AMZ5; DUE REPLACEMENT OF SEAT TRACK.
- [SDR SWAA2025110317055](https://openairdocs.org/sdr/SWAA2025110317055.md): Shield · corroded · Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD BS 500-500A, S27R WL 156. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV -.
- [SDR SWAA2025110317053](https://openairdocs.org/sdr/SWAA2025110317053.md): Door Frame · cracked · Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, Structure
  > PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. REMOVED AND REPLACED PASSENGER CABIN FWD ENTRY DOOR STOP FITTING INTERCOSTAL S16L IAW SRM 51-40-02 AND DWG 141A8180 REV: C.
- [SDR SWAA2025103017185](https://openairdocs.org/sdr/SWAA2025103017185.md): Stringer Clip · cracked · Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727A, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, REV E.
- [SDR SWAA2025103017186](https://openairdocs.org/sdr/SWAA2025103017186.md): Stringer Clip · cracked · Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 727B, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102 REV D.
- [SDR SWAA2025103016913](https://openairdocs.org/sdr/SWAA2025103016913.md): Rib · cracked · Sep 21, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > DURING INSPECTION FOUND CRACK AT NR 4 RIB STA 120.30 STIFFENER NR 2. REPAIRED IAW SRM 55-10-09-2R-5.
- [SDR SWAA2025110316500](https://openairdocs.org/sdr/SWAA2025110316500.md): Scuff Plate · cracked · Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED. RECEIVED NEW AFT CARGO DOOR FWD CORNER SCUFF PLATE ITEM 146A8341-07. IT WILL BE INSTALL ON TASK CARD TTG8Q0157507.
- [SDR SWAA2025110316512](https://openairdocs.org/sdr/SWAA2025110316512.md): Fitting · cracked · Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED FITTING, BS 559+8, LBL 6, WL 148.5. RECEIVED NEW FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02-0G-0, AND AIPC 53-12-11-25 FIG 2.
- [SDR SWAA2025110316718](https://openairdocs.org/sdr/SWAA2025110316718.md): Floorbeam · cracked · Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM, BS 540, LBL 2, WL 208. REMOVED AND INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2025110316719](https://openairdocs.org/sdr/SWAA2025110316719.md): Floorbeam · cracked · Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM BS 540, RBL 2, WL 208. REMOVED AND REINSTALLED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2025103016496](https://openairdocs.org/sdr/SWAA2025103016496.md): Stringer Clip · no discrepancy · Sep 19, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach Fittings
  > FUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2025103016497](https://openairdocs.org/sdr/SWAA2025103016497.md): Stringer Clip · no discrepancy · Sep 19, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach Fittings
  > FUSELAGE STRINGER CLIP BS 727A S15L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2025110316163](https://openairdocs.org/sdr/SWAA2025110316163.md): Pressure Deck · cracked · Sep 18, 2025 · N7862A · Boeing 73779P · Fuselage Main, Structure
  > CRACK NOTED ON LEFT HORIZONTAL PRESSURE DECK WEB BS 673, LBL 32, WL 202.5. L: 0.4. REPAIRED THE PRESSURE DECK AND REMOVED & REPLACED ALL SHORT AND HIGH FASTENERS AND INSTALLED MISSING COLLARS AT THE REPAIR AREA AS A CORRECTION FOR STEP 10, ITEM 1 IAW SRM 53-
- [SDR SWAA2025103015048](https://openairdocs.org/sdr/SWAA2025103015048.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015049](https://openairdocs.org/sdr/SWAA2025103015049.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015050](https://openairdocs.org/sdr/SWAA2025103015050.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015052](https://openairdocs.org/sdr/SWAA2025103015052.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241BF REPLACED WITH A NEW FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025103015054](https://openairdocs.org/sdr/SWAA2025103015054.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015057](https://openairdocs.org/sdr/SWAA2025103015057.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015056](https://openairdocs.org/sdr/SWAA2025103015056.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015058](https://openairdocs.org/sdr/SWAA2025103015058.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW DWG 144A5810 0123.
- [SDR SWAA2025103015051](https://openairdocs.org/sdr/SWAA2025103015051.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015047](https://openairdocs.org/sdr/SWAA2025103015047.md): Floor Panel · pulled · Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor Panel
  > FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS FABRICATION OF NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025110415045](https://openairdocs.org/sdr/SWAA2025110415045.md): Skin · no discrepancy · Sep 15, 2025 · N7862A · Boeing 73779P · Leading Edge Devices
  > SUSPECT CRACK RT WING NR 5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING, SLAT STATION 85.19. HFEC INSPECTED RT WING #5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING SLAT STATION 85.19 IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2025110415026](https://openairdocs.org/sdr/SWAA2025110415026.md): Inlet · pulled · Sep 15, 2025 · N7862A · Boeing 73779P · Nacelle/Pylon, Main Frame
  > PULLED THROUGH FASTENERS 2 O' CLOCK POSITION ON RIGHT INLET COWL OUTER LIP SKIN. REMOVED AND REPLACED RT INLET COWL OUTER LIP SKIN IAW SRM 54-10-01-1A-2 AND SRM 51-40-02. ACCOMPLISHED NDI INSPECTION IAW NDTM PART 6; 51-00-00. REMOVED AND REPLACED NR 2 ENGI
- [SDR SWAA2025040720513](https://openairdocs.org/sdr/SWAA2025040720513.md): Door · warning light · Apr 1, 2025 · N7862A · Boeing 73779P · Door Warning System
  > CLIMBING OUT GOT AFT ENTRY DOOR LT; RAN QRH HANDLE HAD MOVED; LT WENT OUT; DOOR LT CAME BACK ON A 2ND TIME ON FINAL; AT DIVERT CITY OF KLIT.<[01] REMOVED DEBRIS FROM AFT ENTRY DOOR EXTERIOR HANDLE RECESS & ACCOMPLISHED OPEN/CLOSE WITH THE INTERIOR & EXTERIORDO
- [SDR SWAA2025010783480](https://openairdocs.org/sdr/SWAA2025010783480.md): Battery Pack · no test · Jan 6, 2025 · N7862A · Boeing 73779P · Emergency Lighting
  > ALL LIGHT RELATED TO BATTERY PACK M2335 FAIL TEST. REPLACED EMERGENCY BATTERY PACK. PERFORMED GOOD TEST PER AMM 33-51-06-960-805.
- [SDR SWAA2025010783482](https://openairdocs.org/sdr/SWAA2025010783482.md): Lamp · failed · Jan 6, 2025 · N7862A · Boeing 73779P · Emergency Lighting
  > LEFT AND RIGHT OVERWING ESCAPE GROUND ILLUMINATION FAIL EMERGENCY LIGHT TEST (L548) (L547)<[01] REPLACED LAMP TO LEFT AND RIGHT OVERWING ESCAPE (L548) AND (L547) PER AMM 33-51-04-960-801. GOOD TEST.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2025010783481](https://openairdocs.org/sdr/SWAA2025010783481.md): Lamp · inoperative · Jan 6, 2025 · N7862A · Boeing 73779P · Emergency Lighting
  > EMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERVICE DOOR LH SIDE INOP<[01] REPLACED LAMP TO EMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERVICE DOOR LH SIDE PER AMM 33-51-04-960-801. GOOD TEST.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2025010681802](https://openairdocs.org/sdr/SWAA2025010681802.md): Intercostal · cracked · Dec 30, 2024 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > INTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 L/H INTERCOSTAL CRACKED.<[01] PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9.<BR><BR>REMOVED DAMAGED INTERCOSTAL AT STA 927 - 947; STR- 21L/H PER SRM 51-40-02.;[02] FABRICATED; LOCATED AND DR
- [SDR SWAA2024123080862](https://openairdocs.org/sdr/SWAA2024123080862.md): Intercostal · cracked · Dec 26, 2024 · N7862A · Boeing 73779P · Fuselage Miscellaneous Structure
  > INTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 LH INTERCOSTAL IS CRACK.<[01] PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23;[02] PERFORMED EA 24-153-03554'. ADD A REFERENCE TO THE FAULT TTG8Q00XT976.;[03] VERIFIED PERFORMED EA 24-153-03554'. ADD A REFE
- [SDR SWAA2024123080858](https://openairdocs.org/sdr/SWAA2024123080858.md): Skin · cracked · Dec 26, 2024 · N7862A · Boeing 73779P · Fuselage Main, Plate/Skin
  > INTERNAL DAMAGE AT STA 927 STR 21 LH CRACK. PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23. PERFORMED EA 24-153-03554'. ADD A REFERENCE TO THE FAULT TTG8Q00XT976.
- [SDR SWAA2024102852533](https://openairdocs.org/sdr/SWAA2024102852533.md): Seal · cracked · Oct 24, 2024 · N7862A · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STABILIZER UPPER STAB TO BODY SLIDING SEAL IS CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]

Next page: https://openairdocs.org/aircraft/N7862A/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 = 'N7862A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7862A/reports

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