# Service difficulty reports: N8662F

A list on [N8662F](https://openairdocs.org/aircraft/N8662F.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 3 · 114 reports

- [SDR SWAA2026100604108](https://openairdocs.org/sdr/SWAA2026100604108.md): Megaphone · inoperative · Oct 2, 2026 · N8662F · Boeing 7378H4 · Emergency Equipment
  > AFT MEGAPHONE INOPERATIVE. R & R MEGAPHONE AMM 25-64-00.
- [SDR SWAA2026073161997](https://openairdocs.org/sdr/SWAA2026073161997.md): Lamp · inoperative · Jul 27, 2026 · N8662F · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AT R1 DOOR INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LAMP AT R1 DOOR IAW AMM 33-51-04. OPS. CHECKED GOOD.
- [SDR SWAA2026072884652](https://openairdocs.org/sdr/SWAA2026072884652.md): Lens · loose · Jul 24, 2026 · N8662F · Boeing 7378H4 · Emergency Lighting
  > MID CABIN EMERGENCY EXIT SIGN LENS WILL NOT STAY ATTACHED. SECURED PER M-EA M-24-133-00396
- [SDR SWA2026F00001](https://openairdocs.org/sdr/SWA2026F00001.md): Cap · leaking · Jul 20, 2026 · N8662F · Boeing 7378H4 · Fuel Storage
  > OTS - DIV- CAPTAIN REPORTS FUEL IMBALANCE. LOSING FUEL FROM #2 TANK_ INSPECTED AC FOR FUEL LEAKS NONE FOUND. PERFORMED FQIS BITE IAW FIM 28-41 TASK 801 NO FAULTS FOUND. STICK READINGS SHOW 6660LBS IN #1 AND #2 TANKS WITH FLIGHT DECK READINGS SHOWING #1 TANK AT
- [SDR SWAA2026072447702](https://openairdocs.org/sdr/SWAA2026072447702.md): Tank Unit · leaking · Jul 20, 2026 · N8662F · Boeing 7378H4 · Fuel Quantity Indicator
  > DURING CLIMB NR 2 FUEL TANK QUANTITY DECREASED TO OVER 1000 LBS IMBALANCE WITH 3000 LBS OF FUEL IN THE CENTER INSPECTED AC FOR FUEL LEAKS NONE FOUND. PERFORMED FQIS BITE IAW FIM 28-41 TASK 801 NO FAULTS FOUND. STICK READINGS SHOW 6660LBS IN NR 1 AND 2 TANKS WI
- [SDR SWAA2026072427046](https://openairdocs.org/sdr/SWAA2026072427046.md): Compensator · faulted · Jul 20, 2026 · N8662F · Boeing 7378H4 · Fuel Quantity Indicator
  > DURING CLIMB NR 2 FUEL TANK QTY DECREASED TO OVER 1000 LBS IMBALANCE WITH 3000 LBS OF FUEL IN THE CENTER INSPECTED ACFT FOR FUEL LEAKS NONE FOUND. PERFORMED FQIS BITE IAW FIM 28-41 TASK 801 NO FAULTS FOUND. STICK READINGS SHOW 6660LBS IN NR 1 AND NR 2 TANKS W
- [SDR SWAA2026072407018](https://openairdocs.org/sdr/SWAA2026072407018.md): Tank Unit · leaking · Jul 20, 2026 · N8662F · Boeing 7378H4 · Fuel Quantity Indicator
  > DURING CLIMB, NR 2 FUEL TANK QTY DECREASED TO OVER 1000 LBS IMBALANCE WITH 3000 LBS OF FUEL IN THE CENTER. INSPECTED ACFT FOR FUEL LEAKS NONE FOUND. PERFORMED FQIS BITE IAW FIM 28-41, TASK 801, NO FAULTS FOUND. STICK READINGS SHOW 6660LBS IN NR 1 & 2 TANKS W
- [SDR SWAA2026072426571](https://openairdocs.org/sdr/SWAA2026072426571.md): Tank Unit · leaking · Jul 20, 2026 · N8662F · Boeing 7378H4 · Fuel Quantity Indicator
  > DURING CLIMB NR 2 FUEL TANK QUANTITY DECREASED TO OVER 1000 LBS IMBALANCE WITH 3000 LBS OF FUEL IN THE CENTER INSPECTED ACFT FOR FUEL LEAKS NONE FOUND. PERFORMED FQIS BITE IAW FIM 28-41 TASK 801 NO FAULTS FOUND. STICK READINGS SHOW 6660LBS IN NR 1 & 2 TANKS WI
- [SDR SWAA2026011260358](https://openairdocs.org/sdr/SWAA2026011260358.md): Lens · missing · Jan 11, 2026 · N8662F · Boeing 7378H4 · Emergency Lighting
  > FORWARD FACING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED FWD EMERGENCY EXIT LENS IAW SIP.
- [SDR SWAA2025121544127](https://openairdocs.org/sdr/SWAA2025121544127.md): Handle · loose · Dec 9, 2025 · N8662F · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR, DOOR ASSIST HANDLE LOOSE. TIGHTENED FWD ON DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802 STEPS 3.G.(2). (A-D).
- [SDR SWAA2025121544125](https://openairdocs.org/sdr/SWAA2025121544125.md): Handle · loose · Dec 9, 2025 · N8662F · Boeing 7378H4 · Service Doors
  > SERVICE DOOR FWD & ON DOOR ASSIST HANDLE LOOSE. TIGHTENED FWD ON DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802 STEPS 3.G.(2). (A-D).
- [SDR SWAA2025121247721](https://openairdocs.org/sdr/SWAA2025121247721.md): Cover · broken · Dec 9, 2025 · N8662F · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT ASSY COVER LOOSE. UPON FURTHER INVESTIGATION, THE RT OVERWING EMERGENCY LIGHT ASS COVER FOUNDS TO BE BROKEN. R & R THE RT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-01-960-802, STEPS C.(1)-(4);(5).(D);(6);(11);(12). OPS CHEC
- [SDR SWAA2025121244126](https://openairdocs.org/sdr/SWAA2025121244126.md): Cover · broken · Dec 9, 2025 · N8662F · Boeing 7378H4 · Emergency Lighting
  > RH OWE EMERGENCY LIGHT ASSEMBLY COVER LOOSE. UPON FURTHER INVESTIGATION THE RT OVERWING EMERGENCY LIGHT ASSEMBLY COVER FOUNDS TO BE BROKEN. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01-960-802, STEPS C.(1)-(4);(5).(D);(6);(11);
- [SDR SWAA2025121247720](https://openairdocs.org/sdr/SWAA2025121247720.md): Sign · miswired · Dec 8, 2025 · N8662F · Boeing 7378H4 · Light System Wiring
  > AFT RT EMERGENCY EXIT LIGHT AT BS 639 IS INOPERATIVE. UPON FURTHER INVESTIGATION; FOUND AFT RT OVERWING EXIT EMERGENCY LIGHT SIDEWALL SIGN CONNECTED TO WIRING FOR OVERWING EXIT DOOR HEATERS. RECONNECTED AFT RT OVERWING EXIT EMERGENCY LIGHT SIDEWALL SIGN AND O
- [SDR SWAA2025121244124](https://openairdocs.org/sdr/SWAA2025121244124.md): Sign · miswired · Dec 8, 2025 · N8662F · Boeing 7378H4 · Light System Wiring
  > AFT RT EMERGENCY LIGHT AT BS 639 IS INOPERATIVE. UPON FURTHER INVESTIGATION, FOUND AFT RT OVERWING EXIT EMERGENCY LIGHT SIDEWALL SIGN CONNECTED TO WIRING FOR OVERWING EXIT DOOR HEATERS. RECONNECTED AFT RT OVERWING EXIT EMERGENCY LIGHT SIDEWALL SIGN & OVERWIN
- [SDR SWAA2025102025454](https://openairdocs.org/sdr/SWAA2025102025454.md): Sign · missing · Oct 17, 2025 · N8662F · Boeing 7378H4 · Emergency Lighting
  > THE EXIT SIGN MID CABIN OVERHEAD IS MISSING. INSTALLED MISSING MID CABIN OVERHEAD EXIT SIGN IN REFERENCE TO AMM 33-51-01
- [SDR SWAA2025081404179](https://openairdocs.org/sdr/SWAA2025081404179.md): Girt Bar · out of adjust · Aug 14, 2025 · N8662F · Boeing 7378H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE GIRT BAR REQUIRES REPLACEMENT. R & R FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2024122680799](https://openairdocs.org/sdr/SWAA2024122680799.md): Lens · loose · Dec 25, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > CEILING EMERGENCY EXIT LENS FELL OFF<[01] REINSTALLED IAW AMM 33-51-03
- [SDR SWAA2024110856424](https://openairdocs.org/sdr/SWAA2024110856424.md): Access Panel · delaminated · Nov 4, 2024 · N8662F · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 193AL HAS AN AREA OF DELAMINATION ON LOWER SIDE FWD EDGE AS MARKED<[01] OK TO CONT. PER TLD PER SRM 53-40-70-1A-1;[02] REINSPECT FOR TAPE REQ EVERY 8 DAYS;[03] QC CONCURS THAT THE ACTIONS TAKEN WERE APPROPRIATE; ARE IN ACCORDANCE WITH THE APPLICABLE SRM;
- [SDR SWAA2024102852124](https://openairdocs.org/sdr/SWAA2024102852124.md): Light · loose · Oct 23, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > 8 ABC EMERGENCY LIGHT LOOSE<[01] TIGHTENED EMERGENCY EXIT LIGHT AT 8 ABC IAW AMM 33-51-01.
- [SDR SWAA2024102351292](https://openairdocs.org/sdr/SWAA2024102351292.md): Sign · loose · Oct 20, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE EMERGENCY EXIT SIGN<[01] 2032223
- [SDR SWAA2024102350731](https://openairdocs.org/sdr/SWAA2024102350731.md): Skin · delaminated · Oct 19, 2024 · N8662F · Boeing 7378H4 · Trailing Edge Flaps
  > L/H O/B AFT FLAP HAS DELAM AREA INBD END LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP PER AMM 27-51-22.;[02] INSTALLED L/H O/B AFT FLAP UP TO RIGGING AND ADJUSTMENT PER MM 27-51-22;[03] INSTALLED L/H O/B AFT FLAP UP TO AND INCLUDING STEP 3(F)(5) RIGGING AND AD
- [SDR SWAA2024091135530](https://openairdocs.org/sdr/SWAA2024091135530.md): Cover · detached · Sep 8, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > AFT FACING EXIT/SALIDA SIGN FELL OFF.<[01] RE-INSTALLED MID-CABIN EMERGENCY EXIT SIGN LENS COVER PER AMM 33-51-03.
- [SDR SWAA2024071211763](https://openairdocs.org/sdr/SWAA2024071211763.md): Retaining Ring · missing · Jul 11, 2024 · N8662F · Boeing 7378H4 · Emergency Equipment
  > RETAINING RING MISSING ON FWD SERVICE GIRTH BAR<[01] REINSTALLED BAR LOCK ON FWD SERVICE DOOR PER AMM 25-66-01.
- [SDR SWAA2024022050216](https://openairdocs.org/sdr/SWAA2024022050216.md): Battery Pack · inoperative · Feb 8, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT DOOR SIGN LIGHT INOP<[01] R&R BATTERY PACK AND CHARGER ASSY FOR POWER SUPPLY M1695 IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM 33-51-06. SEE TTG8Q00RF7WN FOR PARTS DATA.;[02] INSPECTION C/W
- [SDR SWAA2024022050214](https://openairdocs.org/sdr/SWAA2024022050214.md): Battery Pack · inoperative · Feb 8, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > RH OVERWING EXIT EMERGENCY EXIT SIGN LIGHTS INOP<[01] R&R BATTERY PACK AND CHARGER ASSY FOR POWER SUPPLY M1695 IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM 33-51-06.;[02] PARTS UPDATE;[03] INSPECTION C/W
- [SDR SWAA2024022050215](https://openairdocs.org/sdr/SWAA2024022050215.md): Battery Pack · inoperative · Feb 8, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT BS 709 RBL 18 INOP<[01] R&R M1671 BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM 33-51-06.;[02] INSPECTION C/W
- [SDR SWAA2024022050217](https://openairdocs.org/sdr/SWAA2024022050217.md): Battery Pack · inoperative · Feb 8, 2024 · N8662F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT AISLE LIGHT INOP AT BS500B+3 RBL 18<[01] R&R BATTERY PACK FOR POWER SUPPLY M1676 IAW AMM 33-51-06.;[02] INSPECTION C/W
- [SDR SWAA2024022049542](https://openairdocs.org/sdr/SWAA2024022049542.md): Fairing · delaminated · Feb 6, 2024 · N8662F · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING # 7 FLAP TRACK AFT CANOE FAIRING IS DELAMINATED ON UPPER AFT SURFACE (MARKED)<[01] REMOVED DALAMINATED #7 FLAP TRACK AFT FAIRING AND INSTALLED NEW FAIRING PER AMM 27-51-28.;[02] REMOVED DALAMINATED #7 FLAP TRACK AFT FAIRING AND INSTALLED NEW FAIRING
- [SDR SWAA2024022048619](https://openairdocs.org/sdr/SWAA2024022048619.md): Seat Track · cracked · Feb 4, 2024 · N8662F · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN APPROX STA 727A + 19 SEAT TRACK SUPPORT CRACKED AT RBL 46 O/B AFT HOLE. HOLE SIZE IS NOW.262<[01] REMOVED DAMAGE PER SRM 53-40-51-2R-1 REPAIR1.;[02] REMOVED DAMAGE PER SRM 53-40-51-2R-1 REPAIR1. INSPECTION C/W.;[03] PERFORMED HFEC INSPECTION OF THE CUT
- [SDR SWAA2024022047366](https://openairdocs.org/sdr/SWAA2024022047366.md): Gusset · cracked · Jan 31, 2024 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN STA 727B LOWER GUSSET CRACKED AT RBL 45 FWD OF SEAT TRACK HI-LOCK NUT LOWER SURFACE<[01] REMOVED CRACKED GUSSET IAW SRM 51-40-02.;[02] ACCOMPLISHED NDT ON ALL OPEN HOLES COMMON TO THE GUSSET PER NDT MANUAL PART 6 CH.51-00-00 PROCEDURE 16. ONE DEFECT NOTE
- [SDR SWAA2024022047365](https://openairdocs.org/sdr/SWAA2024022047365.md): Floor Support · cracked · Jan 31, 2024 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CRACKED STA 540 LBL-1<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.;[02] ANSWERED MEASUREMENTS;[03] C/W C/A #1 AND #2;[04] UPDATED MEASUREMENT QUESTIONS. FAULT IS COMPLETE;[05] FAULT IS COMPLETE SEE CA 1; 2; & 3.
- [SDR SWAA2024022047364](https://openairdocs.org/sdr/SWAA2024022047364.md): Floor Support · cracked · Jan 31, 2024 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CRACKEC STA 540 RBL 1<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT AT STA 540 RBL 1 PER SRM 51-40-02.;[02] EDITED PARTS INFO ONLY.;[03] C/W C/A #1 AND #2;[04] UPDATED MEASUREMENT QUESTION
- [SDR SWAA2024022047374](https://openairdocs.org/sdr/SWAA2024022047374.md): Rib · cracked · Jan 31, 2024 · N8662F · Boeing 7378H4 · Wing, Rib/Bulkhead
  > LEFT WING TRAILING EDGE RIB IS CRACKED AT DEFLECTION RIB PANEL.<[01] RIB WAS REPLACED ON NR TTG8Q00R8TCV LINE #1207;[02] VERIFIED RIB WAS REPLACED ON NR TTG8Q00R8TCV LINE #1207
- [SDR SWAA2024022046649](https://openairdocs.org/sdr/SWAA2024022046649.md): Skin · delaminated · Jan 30, 2024 · N8662F · Boeing 7378H4 · Trailing Edge Flaps
  > R/H O/B AFT FLAP REQUIRES REPLACEMENT DUE TO DELAMINATION ON I/B LOWER CORNER (MARKED)<[01] OK TO INSTALL R/H OB FLAP.;[02] REMOVAL AND REPLACEMENT OF R/H OUTBOARD AFT FLAP PARTS IS ACCOMPLISHED ON TTG8Q00R7YCX;[03] VERIFIED R/H OUTBOARD AFT FLAP PARTS IS ACC
- [SDR SWAA2024022046888](https://openairdocs.org/sdr/SWAA2024022046888.md): Web · cracked · Jan 30, 2024 · N8662F · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING DEFLECTION RIB LOWER ATTACH BRACKET CRACKED OTBD. UPPER CORNER.<[01] REMOVED WEB FOR REPLACEMENT.;[02] REMOVED WEB FOR REPLACEMENT PER SRM 51-40-02.;[03] REPLACED BRACKET PER SRM 51-40-02;[04] INSPECTION C/W
- [SDR SWAA2024022046148](https://openairdocs.org/sdr/SWAA2024022046148.md): Skin · delaminated · Jan 29, 2024 · N8662F · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED; INBOARD UPPER SURFACE.<[01] PARTS UPDATE;[02] REMOVAL AND REPLACEMENT TO BE ACCOMPLISHED ON NON-ROUTINE CARD # TTG8Q00R8PNW;[03] VERIFIED REMOVAL AND REPLACEMENT TO BE ACCOMPLISHED ON NON-ROUTINE CARD # T
- [SDR SWAA2023072080279](https://openairdocs.org/sdr/SWAA2023072080279.md): Light · inoperative · Jul 19, 2023 · N8662F · Boeing 7378H4 · Emergency Lighting
  > AFT LEFT SLIDE EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04
- [SDR SWAA2023071176794](https://openairdocs.org/sdr/SWAA2023071176794.md): Light · inoperative · Jul 10, 2023 · N8662F · Boeing 7378H4 · Emergency Lighting
  > AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04
- [SDR SWAA2023031311288](https://openairdocs.org/sdr/SWAA2023031311288.md): Battery Pack · inoperative · Mar 1, 2023 · N8662F · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP LEFT SIDE BINS<[01] REMOVED SAND REPLACED 4 EMERGENCY BATTERY PACKS.ROW 7;12; 20 ABC AND FOWARD CENTER COMPARTMENT. OPS CHECKS GOOD PER MM 33-51-00;[02] REMOVED AND REPLACED 4 EMERGENCY BATTERY PACKS.ROW 7;12; 20 ABC AND FOWARD CE
- [SDR SWAA2023031311073](https://openairdocs.org/sdr/SWAA2023031311073.md): Bracket · cracked · Feb 28, 2023 · N8662F · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING; 'L' BRACKET CRACKED ON I/B SIDE OF MAIN FLAP ROLLERS CASTING BETWEEN I/B AND O/B MAIN FLAPS (MARKED)<[01] REMOVED AND REPLACED ?L? BRACKET I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2023031308067](https://openairdocs.org/sdr/SWAA2023031308067.md): Shield · corroded · Feb 22, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO SHIELD AFT OF THE FWD CARGO DOOR FROM STA 492.4 TO STA 500A HAS CORROSION.<[01] REMOVED CORROSION ON TRANSITION ANGLE SHIELD; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] INSTALLED NEW FWD CARGO TRANSITION ANGLE SHIELD FROM STA 492.4 TO STA
- [SDR SWAA2023031301395](https://openairdocs.org/sdr/SWAA2023031301395.md): Beam · corroded · Feb 9, 2023 · N8662F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT GALLEY FLOOR STRUCTURE STA. 947 FLOOR-BEAM LBL 25.5 ON FWD FLANGE HAS CORROSION AROUND GALLEY NUTPLATE BRACKET.<[01] REMOVED DAMAGE I.A.W SRM 53-70-51-2R-8. MEASURED REMAINING THICKNESS TO BE 0.1375'.05] FABRICATED FILLER IAW SRM 53-70-51-2R-8. OK TO INSTA
- [SDR SWAA2023031301396](https://openairdocs.org/sdr/SWAA2023031301396.md): Scuff Plate · cracked · Feb 9, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO FORWARD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED SCUFF PLATE BY OUT SIDE VENDOR PO# P6373587-1 & TO BE INSTALLED ON ROUTINE CARD # TTG8R007BGXS AS PER AMM 53-11-02.;[02] INSP C/W
- [SDR SWAA2023031301397](https://openairdocs.org/sdr/SWAA2023031301397.md): Scuff Plate · cracked · Feb 9, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED.<[01] REPAIRED SCUFF PLATE BY OUT SIDE VENDOR PO# P6378473-1 & TO BE INSTALLED ON ROUTINE CARD # TTG8R007BGV3 AS PER AMM 53-11-02.;[02] INSP C/W
- [SDR SWAA2023031300312](https://openairdocs.org/sdr/SWAA2023031300312.md): Beam · corroded · Feb 8, 2023 · N8662F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT GALLEY FLOOR STRUCTURE STA. 947 FLOOR-BEAM RBL 50; CORROSION AROUND GALLEY NUTPLATE BRACKET.<[01] REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[17] OK TO INSTALL REPAIR PARTS PER SRM 53-70-51-2R-5 AND EA 23-153-00520.;[18] INSTALL
- [SDR SWAA2023031399800](https://openairdocs.org/sdr/SWAA2023031399800.md): Angle · corroded · Feb 6, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA 727F THRU 727G..<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENTS.;[03] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.030'). TRANSITION ANGLE IS OUT OF
- [SDR SWAA2023031399798](https://openairdocs.org/sdr/SWAA2023031399798.md): Angle · corroded · Feb 6, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA 727G THRU 747.<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENTS.;[03] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TRANSITION ANGLE IS OUT OF LI
- [SDR SWAA2023031399778](https://openairdocs.org/sdr/SWAA2023031399778.md): Angle · corroded · Feb 6, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR R/H TRANSITION ANGLE BETWEEN STA 500H TO 500I HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES.<[01] FWD CARGO R/H TRANSITION ANGLE IS OUT OF LIMITS BETWEEN STA 500H AND 500I PER SRM 53-00-53-1A-2.;[02] FWD CARGO R/H TRANSITION ANGLE BETWEEN 500
- [SDR SWAA2023031399779](https://openairdocs.org/sdr/SWAA2023031399779.md): Strap · corroded · Feb 6, 2023 · N8662F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR PANEL ATTACH STRAP HAS CORROSION STA 767+6.<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENTS.;[03] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.045'). STRAP IS OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED A

Next page: https://openairdocs.org/aircraft/N8662F/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 = 'N8662F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8662F/reports

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