# Service difficulty reports: N8669B

A list on [N8669B](https://openairdocs.org/aircraft/N8669B.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 2 · 65 reports

- [SDR SWAA2026051903519](https://openairdocs.org/sdr/SWAA2026051903519.md): Bulb · burned out · May 16, 2026 · N8669B · Boeing 7378H4 · Emergency Lighting
  > AFT RIGHT UPPER INTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT 1 BULB OUT. RELAMPED AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-01-960-801.
- [SDR SWAA2026033184153](https://openairdocs.org/sdr/SWAA2026033184153.md): Megaphone · inoperative · Mar 28, 2026 · N8669B · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY MEGAPHONE INOP. REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-64-00. OPS CHECK GOOD
- [SDR SWAA2026021267550](https://openairdocs.org/sdr/SWAA2026021267550.md): Lamp · inoperative · Feb 4, 2026 · N8669B · Boeing 7378H4 · Emergency Lighting
  > R2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IN THE EMERGENCY LIGHT AND OPS CHECKED GOOD IAW AMM 33-54-01.
- [SDR SWAA2025061379494](https://openairdocs.org/sdr/SWAA2025061379494.md): Egt Indication · illuminated · Jun 7, 2025 · N8669B · Boeing 7378H4 · Engine Temperature Indicating System
  > AFTER ROTATION THE NUMBER 2 ENGINE EXCEEDED THE EGT LIMITATION. THE EGT WAS SOLID RED AND WE SAW 906 COMPLETED QRH ENGINE CONSISTENTLY RAN 50-60 HIGHER THAN NUMBER 1 ENGINE BUT WITHIN NORMAL PARAMETER<[01] C/W EA 25-171-01518;[02] ENTERING CORRECT SELECT REFER
- [SDR SWAA2024112161105](https://openairdocs.org/sdr/SWAA2024112161105.md): Light · loose · Nov 18, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > MID CABIN CEILING EMERGENCY EXIT SIGN IS LOOSE<[01] RE ADJUST EXIT LIGHT ASSEMBLY PER AMM 33-51-01.
- [SDR SWAA2024071613054](https://openairdocs.org/sdr/SWAA2024071613054.md): Flap System · malfunctioned · Jul 15, 2024 · N8669B · Boeing 7378H4 · Trailing Edge Flap Control System
  > FLAPS DID NOT EXTEND BEYOND FLAPS 5 WHILE ON APPROACH; FLAP HANDLE IN THE FLAPS 30 POSITION<[01] REF LOG 2595068 FLAP OVER SPEED - PERFORMED FSEU BITE PER FIM 27-51 TASK 801; NO EXISTING FAULTS FOUND; NO LAST LEG FAULT HISTORY. PERFORMED FLAP TRANSMISSION TOR
- [SDR SWAA2024071611221](https://openairdocs.org/sdr/SWAA2024071611221.md): Battery Pack · inoperative · Jul 11, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT M01673 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
- [SDR SWAA2024071511218](https://openairdocs.org/sdr/SWAA2024071511218.md): Battery Pack · inoperative · Jul 11, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT M01695 WILL NOT CHARGE<[01] REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[03] VERIFIED STEPS 1
- [SDR SWAA2024071511220](https://openairdocs.org/sdr/SWAA2024071511220.md): Battery Pack · inoperative · Jul 11, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT M01672 WILL NOT CHARGE<[01] REMOVED AND REPLACED IAW [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] REMOVED AND REPLACED IAW AMM 33-51-06-960-805-NG CHECK OPS GOOD;[03] REMOVED AND REPLACED BATTE
- [SDR SWAA2024071511222](https://openairdocs.org/sdr/SWAA2024071511222.md): Battery Pack · inoperative · Jul 11, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT M01675 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
- [SDR SWAA2024071511219](https://openairdocs.org/sdr/SWAA2024071511219.md): Battery Pack · inoperative · Jul 11, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT M02816 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
- [SDR SWAA2024071511109](https://openairdocs.org/sdr/SWAA2024071511109.md): Lens · worn · Jul 10, 2024 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON G1 GALLEY IS WORN<[01] REMOVED AND REPLACED G1 GALLEY EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-802-NG STEPS 3E(1(A2)) AND 3E(2(G2)) OP CHECK GOOD<BR>A-TAG; WN31349;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
- [SDR SWAA2024071110063](https://openairdocs.org/sdr/SWAA2024071110063.md): Erosion Shield · delaminated · Jul 7, 2024 · N8669B · Boeing 7378H4 · Wing Main, Frame Structure
  > (A150-001) CORNER DELAMINATED ON LEFT WING L/E PANEL 521TB.<[01] BONDED LOOSE EROSION STRIP IAW SRM 57-41-01-2R-6;[02] AUDIT
- [SDR SWAA2024071505882](https://openairdocs.org/sdr/SWAA2024071505882.md): Plate · failed · Jun 26, 2024 · N8669B · Boeing 7378H4 · Passenger/Crew Doors
  > (A-221 DOT 38); FWD WET AREA L1 DOOR IS SAGGING/ FAILED GAP CHECK BETWEEN DOOR AND DOOR SKIN CUTOUT<[01] REMOVED AND REPLACED UPPER AND LOWER SERRATED PLATE ASSEMBLIES; AND GUIDE ARM IAW SRM 51-40-02-0G-0 AND TASK CARD 752-RCB-01-01 FAULT TTG8R007P3ND. L1 DOOR
- [SDR SWAA2023080986918](https://openairdocs.org/sdr/SWAA2023080986918.md): Slide · out of adjust · Aug 7, 2023 · N8669B · Boeing 7378H4 · Escape Slide
  > AFT LEFT SERVICE DOOR SLIDE HAS A BLACK ELECTRICAL CORD HANGING OUT<[01] UPON INSPECTION FOUND TO BE SLIDE TEST CONNECTOR; SECURED CONNECTOR BACK INTO SLIDE SLEEVE AS REQUIRED REF S.I.P AND AMM 25-66-01
- [SDR SWAA2023061956956](https://openairdocs.org/sdr/SWAA2023061956956.md): Slat · cracked · Jun 7, 2023 · N8669B · Boeing 7378H4 · Leading Edge Devices
  > #4 SLAT MID FLEX SKIN CRACKED<[01] REMOVED AND REPLACED FLEX SEAL (SKIN) IAW SRM 51-40-02
- [SDR SWAA2023061956953](https://openairdocs.org/sdr/SWAA2023061956953.md): Battery Pack · inoperative · Jun 7, 2023 · N8669B · Boeing 7378H4 · Emergency Lighting
  > SEVERAL CABIN EMERGENCY LIGHTS INOP. BOTH SIDES BULL NOSE LIGHTS<[01] REMOVED AND REPLACED 5 EACH BATTERY PACKS IN CABIN FOR BULL NOSE EMERGENCY LIGHTS PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00;[02] REMOVED AND REPLACED 5 EACH BATTERY PACKS IN CABIN FOR
- [SDR SWAA2023061952600](https://openairdocs.org/sdr/SWAA2023061952600.md): Angle · cracked · May 26, 2023 · N8669B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) IS CRACKED AT STA 727J +9. MARKED.<[01] AFT CARGO L/H TRANSITION ANGLE AT STA 727J +9 TO BE REPLACED ON FAULT TTG8Q00L9SR4.;[02] VERIFIED.
- [SDR SWAA2023061952611](https://openairdocs.org/sdr/SWAA2023061952611.md): Angle · corroded · May 26, 2023 · N8669B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) HAS CORROSION AROUND THE FASTENER HOLES. LOCATED AT STA 727J +2; +6; +13 AND +14. MARKED. AFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) HAS CORROSION AROUND THE FASTENER HOLES. LOCAT
- [SDR SWAA2023061952595](https://openairdocs.org/sdr/SWAA2023061952595.md): Splice · corroded · May 26, 2023 · N8669B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT CARGO FLOOR STRUCTURE: CORROSION ON THE UPPER SURFACE OF FLOOR SUPPORT BEAM. LOCATED AT STA 787 RBL 15 ABOVE STR 26R. MARKED. SEE ATTACHED IMAGES.<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENTS.;[03] REMOVED CORROSION FROM AREA PER SR
- [SDR SWAA2023061952609](https://openairdocs.org/sdr/SWAA2023061952609.md): Web · corroded · May 26, 2023 · N8669B · Boeing 7378H4 · Fuselage Main, Structure
  > AFT CARGO FLOOR STRUCTURE: CARGO DOOR THRESHOLD SUPPORT WEB HAS CORROSION ON THE UPPER SURFACE AROUND FASTENERS HOLES STARTING AT STA 787 THROUGH STA 847 RBL 22 TO RBL 26. MARKED (SEE ATTACHED IMAGE.)<[01] DAMAGE OUT OF LIMITS PER SRM 53-60-15-1A-1;[02] CONFIR
- [SDR SWAA2023061952589](https://openairdocs.org/sdr/SWAA2023061952589.md): Floorbeam · corroded · May 25, 2023 · N8669B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT GALLEY STA. 947.5 LBL 24.75 CORROSION AROUND TIE-DOWN FITTING.<[01] CORROSION DAMAGE OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] VERIFIED CORRECTIVE ACTION STEP #1;[03] CUTOUT DAMAGED UPPER CHORD OF FLOOR BEAM AT STA 947.5 FROM LBL 9 TO LBL 42 PER SRM 53-70-5
- [SDR SWAA2023061952592](https://openairdocs.org/sdr/SWAA2023061952592.md): Intercostal · corroded · May 25, 2023 · N8669B · Boeing 7378H4 · Rotorcraft Tail Boom
  > FWD LAV; AFT IB MOUNT AT STA 303.9 LBL 13 HAS CORROSION UNDER NUTPLATE.<[01] REMOVED FWD LAV. AFT I/B MOUNT FITTING AND NUT PLATE PER SRM 51-40-02.<BR>BLENDED OUT CORROSION AT LAV ATTACH FASTENER HOLE PER SRM 51-10-02. FOUND PITTING AND CRACK WITHIN FASTENER H
- [SDR SWAA2023061952583](https://openairdocs.org/sdr/SWAA2023061952583.md): Floorbeam · corroded · May 25, 2023 · N8669B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT GALLEY STA. 987 FLOORBEAM RBL 43 HAS CORROSION AROUND NUT-PLATE HOLE.<[01] CORROSION DAMAGE OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] VERIFIED CORRECTIVE ACTION STEP #1;[03] CUT OUT DAMAGE AREA PER SRM 53-70-51-2R-6 REPAIR ALTERNATIVE 4.;[04] PERFORMED HIGH
- [SDR SWAA2023061952037](https://openairdocs.org/sdr/SWAA2023061952037.md): Flap · delaminated · May 24, 2023 · N8669B · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED R/H WING 'O/B AFT FLAP' IAW AMM 27-51-22.;[02] INSTALLED SERVICEABLE R/H O/B AFT FLAP REF AMM 27-51-22;[03] RII: INSPECTED WORK ACCOMPLISHED IN C/A# 2. THOMAS TESTEMENT (TECHNICI
- [SDR SWAA2023061952038](https://openairdocs.org/sdr/SWAA2023061952038.md): Flap · delaminated · May 24, 2023 · N8669B · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED L/H WING; ' O/B AFT FLAP '; IAW AMM 27-51-22.;[02] ACCOMPLISHED INSTALLATION OF L/H WING; ' O/B AFT FLAP ' IAW AMM 27-51-22-400-801 UP TO AND INCLUDING STEPS 3. A;B;C;D;E; AND F.
- [SDR SWAA2023061952046](https://openairdocs.org/sdr/SWAA2023061952046.md): Flap · delaminated · May 24, 2023 · N8669B · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE HAS LARGE AREA OF DELAMINATING (MKD)<[01] REMOVED DELAMINATED R/H I/B MAIN FLAP T/E WEDGE PER SRM 51-40-02.;[02] REMOVED PART FROM INVENTORY;[03] OKAY TO CLOSE RIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE;[0
- [SDR SWAA2023061950703](https://openairdocs.org/sdr/SWAA2023061950703.md): Lens · damaged · May 22, 2023 · N8669B · Boeing 7378H4 · Emergency Lighting
  > PASSENGER COMPARTMENT EMERGENCY EGRESS LIGHT FIXTURE AT SEAT ROW 21DEF HAS DAMAGE.<[01] R&R'D EMERGENCY EGRESS LIGHT LENS PER AMM 33-51-03;[02] C/W.
- [SDR SWAA2023020900579](https://openairdocs.org/sdr/SWAA2023020900579.md): Lens · loose · Feb 8, 2023 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LENS CAME OFF<[01] SECURED LENS I/A/W S.I.P.
- [SDR SWAA2023010386686](https://openairdocs.org/sdr/SWAA2023010386686.md): Battery Pack · inoperative · Dec 31, 2022 · N8669B · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING EXIT EMERGENCY LIGHTS INOP.<[01] R/R EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06; OPS CHK GOOD.
- [SDR SWAA2022112374765](https://openairdocs.org/sdr/SWAA2022112374765.md): Seal · cracked · Nov 23, 2022 · N8669B · Boeing 7378H4 · Horizontal Stabilizer Structure
  > R/H HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED R/H HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.
- [SDR SWAA2022112374766](https://openairdocs.org/sdr/SWAA2022112374766.md): Seal · cracked · Nov 23, 2022 · N8669B · Boeing 7378H4 · Horizontal Stabilizer Structure
  > L/H HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED L/H HORIZONTAL STAB UPPER FWD SLIDER SEAL PER AMM 53-31-31.
- [SDR SWAA2022111772470](https://openairdocs.org/sdr/SWAA2022111772470.md): Battery Pack · inoperative · Nov 17, 2022 · N8669B · Boeing 7378H4 · Emergency Lighting
  > ONE INTERIOR EMERGENCY LIGHT INOP AT AFT LT OVHD BIN. EMERGENCY BATTERY PACK M1673 REPLACED. OPS CHECKED NORMAL IAW AMM 33-51-06-960-805.
- [SDR SWAA2022111772469](https://openairdocs.org/sdr/SWAA2022111772469.md): Battery Pack · inoperative · Nov 17, 2022 · N8669B · Boeing 7378H4 · Emergency Lighting
  > INTERIOR EMERGENCY LIGHTS INOP AT L2 DOOR. EMERGENCY BATTERY PACK POS. M1673 WAS REPLACED. PERFORMED OPS CHECK OF THE INTERIOR EMERGENCY LIGHTS AT L2 DOOR AND FOUND NORMAL IAW AMM 33-51-06-960-805.
- [SDR SWAA2022111772468](https://openairdocs.org/sdr/SWAA2022111772468.md): Battery · inoperative · Nov 17, 2022 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS INOP AT R2 DOOR. EMERGENCY BATTERY PACK POS. M1673 WAS REPLACED. PERFORMED OPS CHECK OF THE EXTERIOR EMERGENCY LIGHTS AT R2 DOOR AND FOUND NORMAL
- [SDR SWAA2022111772467](https://openairdocs.org/sdr/SWAA2022111772467.md): Battery · inoperative · Nov 17, 2022 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS INOP AT L2 DOOR. REMOVED AND REPLACED EMERGENCY BATTERY PACK POS M1673. PERFORMED OPS CHECK FOUND NORMAL. REMOVED AND REPLACED EMERGENCY BATTERY PACK POS M1673 PER REF AMM 33-51-06-960-805. PERFORMED OPS CHECK FOUND NORMAL.
- [SDR SWAA2022053112522](https://openairdocs.org/sdr/SWAA2022053112522.md): Pump · faulty · May 27, 2022 · N8669B · Boeing 7378H4 · Engine Fuel Pump
  > ON TAKEOFF WITH TOGA SEL #1 ENG WENT TO 93.5 % N1; #2 ENGINE WENT TO 87.4% N1. ADVANCING (MANUALLY) THE #2 THRUST LEVER DID NOT ADVANCE N1 ABOVE 87.4%. / [01] AFTER INSTALLATION OF FUEL PUMP PACKAGE; #2 ENGINE TAKEOFF POWER IS SATISFACTORY; IAW B737 AMM 71-00-
- [SDR SWAA2021122154220](https://openairdocs.org/sdr/SWAA2021122154220.md): Seal · out of position · Dec 17, 2021 · N8669B · Boeing 7378H4 · Horizontal Stabilizer Structure
  > RT HORIZONTAL STABILIZER AFT UPPER SLIDING SEAL OUT OF CHANNEL; / [01] RE-POSITIONED SEAL PER AMM 27-41-11 STEP G 15
- [SDR SWAA2021110941494](https://openairdocs.org/sdr/SWAA2021110941494.md): Battery Pack · inoperative · Nov 6, 2021 · N8669B · Boeing 7378H4 · Emergency Lighting
  > ELECTRICAL FUMES SMELL AROUND ROW 4; NO ABNORMAL ENG INDICATIONS; / [01] ACCOMPLISHED CONDITIONAL INSP PER AMM 05-51-56 AND FIM 21-00 TASK 806 PARA. C;G;H;I; AND J. NO FAULTS FOUND. COULD NOT DUPLICATE CONDITION. INSPECTED PSUS AND OVERHEAD BINS IN SUSPECT RO
- [SDR SWAA2021110941350](https://openairdocs.org/sdr/SWAA2021110941350.md): Power Supply · inoperative · Nov 6, 2021 · N8669B · Boeing 7378H4 · Emergency Lighting
  > ELECTRICAL FUMES SMELL AROUND ROW 4; NO ABNORMAL ENG INDICATIONS; / [01] ACCOMPLISHED CONDITIONAL INSP PER AMM 05-51-56 AND FIM 21-00 TASK 806 PARA. C;G;H;I; AND J. NO FAULTS FOUND. COULD NOT DUPLICATE CONDITION. INSPECTED PSUS AND OVERHEAD BINS IN SUSPECT RO
- [SDR SWAA2021110137756](https://openairdocs.org/sdr/SWAA2021110137756.md): None · loose · Oct 26, 2021 · N8669B · Boeing 7378H4 · Emergency Lighting
  > EXIT SIGN COVER AFT OF EMERGENCY EXIT DOOR ROW 15 BC IS LOOSE / SECURED EXIT SIGN COVER PER SIP
- [SDR SWAA2021070688442](https://openairdocs.org/sdr/SWAA2021070688442.md): Battery Pack · inoperative · Jun 26, 2021 · N8669B · Boeing 7378H4 · Emergency Lighting
  > FWD GALLEY L/H EMERGENCY LIGHT INOP / R&R FWD GALLEY L/H EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06POS 1: P/N OFF/ON: D717-01-100S/N OFF: 403902 S/N ON: 403902
- [SDR SWAA2021070687237](https://openairdocs.org/sdr/SWAA2021070687237.md): Skin · cracked · Jun 24, 2021 · N8669B · Boeing 7378H4 · Trailing Edge Flaps
  > R/H I/B FLAP I/B END ELEPHANT EAR WORN AND CRACKED LOWER SIDE (MARKED) / REMOVED AND REPLACED THE ELEPHANT EAR ON THE R/H I/B FLAP; I/B END IAW AMM 27-51-11
- [SDR SWAA2021070685445](https://openairdocs.org/sdr/SWAA2021070685445.md): Battery Pack · inoperative · Jun 17, 2021 · N8669B · Boeing 7378H4 · Emergency Lighting
  > AFT SERVICE DOOR EMERGENCY EXIT LIGHT ON HEADER PANEL AND R/H OF G-4 GALLEY DOES NOT ILLUMINATE DURING OPERATIONAL TEST / REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CK GOOD.INSP D54
- [SDR SWAA2021070682757](https://openairdocs.org/sdr/SWAA2021070682757.md): Attach Angle · corroded · Jun 12, 2021 · N8669B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ATTACH ANGLE LOCATED UNDER TRANSITION ANGLE (SHIELD) FROM STA 767 TO 787 AND RBL 21 HAS CORROSION AROUND AND UNDER NUTPLATES. / REMOVED AND REPLACED ATTACH ANGLE UNDER TRANSITION ANGLE (SHIELD) P/N # 146A8127412 ATSMROPER SRM. 51-40-02 (SA-M 326 ATTACHED: A130
- [SDR SWAA2021070680860](https://openairdocs.org/sdr/SWAA2021070680860.md): Intercostal · cracked · Jun 7, 2021 · N8669B · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H WING; INTERCOASTAL CRACKED INBD OF DEFLECTION / REMOVED & REPLACED DAMAGED INTERCOASTAL PER SRM 51-40-02.(SA-M 326 A1303118)
- [SDR SWAA2021070680910](https://openairdocs.org/sdr/SWAA2021070680910.md): Control Panel · faulty · Jun 7, 2021 · N8669B · Boeing 7378H4 · Wing Main, Frame Structure
  > FUEL PANEL OPENING 532DB EDGES ARE NOTCHED FROM PANEL BOLTS / ACCOMPLISHED REPAIR TO FUEL PANEL OPENING 532DB IAW SRM 57-50-01-1A-1 AND SRM 57-20-01-2R-1 REPAIR 1.REFERENCE AP37.8.0615 SRM SUPPLEMENT AVIATION PARTNERS BOEING 57-20-01 REPAIR 1.
- [SDR SWAA2021070680911](https://openairdocs.org/sdr/SWAA2021070680911.md): Control Panel · faulted · Jun 7, 2021 · N8669B · Boeing 7378H4 · Wing Miscellaneous Structure
  > FUEL PANEL OPENING 532PB EDGES ARE NOTCHED FROM PANEL BOLTS / ACCOMPLISHED REPAIR TO FUEL PANEL OPENING 532PB IAW SRM 57-20-01-1A-1 AND SRM 57-20-81-27-1 REPAIR 1.REFERENCE AP37.8.0615 SRM SUPPLEMENT AVIATION PARTNERS BOEING 57-20-01 REPAIR 1.
- [SDR SWAA2021070679831](https://openairdocs.org/sdr/SWAA2021070679831.md): Angle · corroded · Jun 4, 2021 · N8669B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO LEFT T- ANGLE HAS CORROSION ON SURFACE @ STA 500+15 LBL 24 / REMOVED AND REPLACED LEFT TRANSITION ANGLE FROM STA 480 + 9 TO 500 I PER SRM 53-00-53-2R5 AND EA #21-153-01621 REF SRM ID 53-30-53-0I-2 FIG 2 TABLE 2 INTEM 6 143A7501 CHANNEL # BAC1496-444S
- [SDR SWAA2021070679828](https://openairdocs.org/sdr/SWAA2021070679828.md): Angle · corroded · Jun 4, 2021 · N8669B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO RIGHT TRANSITION ANGLE HAS SURFACE CORROSION FROM STA 500 TO STA 500A RBL 35. / REMOVED AND REPLACED FWD CARGO RIGHT TRANSITION ANGLE FROM STA. 500 TO STA. 500A AT RBL 25' PER SRM 51-40-02.(SA-M 326 ATTACHED: A1303121)

Next page: https://openairdocs.org/aircraft/N8669B/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 = 'N8669B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8669B/reports

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