# Service difficulty reports: N8696E

A list on [N8696E](https://openairdocs.org/aircraft/N8696E.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 · 94 reports

- [SDR SWAA2026100226115](https://openairdocs.org/sdr/SWAA2026100226115.md): Flashlight · no test · Sep 28, 2026 · N8696E · Boeing 7378H4 · Emergency Equipment
  > AFT CAPTAIN SIDE FLASHLIGHT NOT TESTING. ALL AFT FA FLASHLIGHTS PUSH TO TEST CHECK GOOD PER AMM 25-64-00
- [SDR SWAA2026090258124](https://openairdocs.org/sdr/SWAA2026090258124.md): Battery · inoperative · Aug 29, 2026 · N8696E · Boeing 7378H4 · Emergency Equipment
  > AFTER FA JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IAW AMM 25-64-00
- [SDR SWAA2026060809165](https://openairdocs.org/sdr/SWAA2026060809165.md): Battery Pack · inoperative · Jun 4, 2026 · N8696E · Boeing 7378H4 · Emergency Lighting
  > FWD SERVICE EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY BATTERY PACK M02816 IAW AMM 33-51-06.
- [SDR SWAA2026052605630](https://openairdocs.org/sdr/SWAA2026052605630.md): Light · loose · May 22, 2026 · N8696E · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT, CEILING. CAPTAINS SIDE ROW 19 WAS FALLING OUT OF SOCKET. SECURED EMERGENCY AREA LIGHT IAW AMM 33-51-03.
- [SDR SWAA2026040284437](https://openairdocs.org/sdr/SWAA2026040284437.md): Light · detached · Mar 29, 2026 · N8696E · Boeing 7378H4 · Emergency Lighting
  > AILSE EMERGENCY LIGHT OVER 12ABC LOOSE/HANGING. OK TO CONTINUE PER MEL 33-15-02. REATTACHED AISLE EMERGENCY LIGHT OVER 12ABC PER SIP OPS CHECK GOOD. NO DEFECT NOTED.
- [SDR SWAA2026010557660](https://openairdocs.org/sdr/SWAA2026010557660.md): Cover · broken · Jan 2, 2026 · N8696E · Boeing 7378H4 · Emergency Lighting
  > ROW 16 OVERHEAD EMERGENCY LIGHT COVER BROKEN. R & R EMERGENCY LIGHT COVER PER AMM. 33-51-03 OPT CHECK GOOD.
- [SDR SWAA2025092615615](https://openairdocs.org/sdr/SWAA2025092615615.md): Handle · loose · Sep 17, 2025 · N8696E · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR LINER ASSIST HANDLE LOOSE. SECURED L1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-11-31.
- [SDR SWAA2025092615611](https://openairdocs.org/sdr/SWAA2025092615611.md): Handle · loose · Sep 17, 2025 · N8696E · Boeing 7378H4 · Service Doors
  > R1 DOOR LINER ASSIST HANDLE LOOSE. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025071791574](https://openairdocs.org/sdr/SWAA2025071791574.md): Battery · failed · Jul 16, 2025 · N8696E · Boeing 7378H4 · Emergency Equipment
  > THE OUTBOARD FLASHLIGHT INSTALLED AT THE RIGHT; AFT FLIGHT ATTENDANTS SEAT FAILED ITS CHECK. THE OUTBOARD FLASHLIGHT INSTALLED AT THE RIGHT AFT FLIGHT ATTENDANTS SEAT FAILED ITS CHECK.<[01] REMOVED AND REPLACED THE BATTERY IN THE OUTBOARD FLASHLIGHT INSTALLED
- [SDR SWAA2025071787659](https://openairdocs.org/sdr/SWAA2025071787659.md): Floor Panel · delaminated · Jul 3, 2025 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231ZF DELAMINATED AND DENTED. REMOVED AND REPLACED FLOOR PANEL 231ZF PER AMM 53-21-00.
- [SDR SWAA2025071787663](https://openairdocs.org/sdr/SWAA2025071787663.md): Bracket · cracked · Jul 3, 2025 · N8696E · Boeing 7378H4 · Wing, Attach Fittings
  > RIGHT WING HAS A BRACKET INBOARD OF SHELF PANEL SUPPORT WEB CRACKED. REMOVED AND REPLACED RH WING BRACKET IB OF SHELF PANEL SUPPORT WEB IAW SRM 51-40-02.
- [SDR SWAA2025071787664](https://openairdocs.org/sdr/SWAA2025071787664.md): Bracket · cracked · Jul 3, 2025 · N8696E · Boeing 7378H4 · Wing, Attach Fittings
  > LEFT WING HAS A BRACKET INBOARD OF SHELF PANEL SUPPORT WEB CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02..
- [SDR SWAA2025071786993](https://openairdocs.org/sdr/SWAA2025071786993.md): Floor Panel · delaminated · Jul 1, 2025 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANELS 241BF; 232RF; 231YF AND 242AF HAVE DENTS/DELAMINATION. REMOVED AND REPLACED PER AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT).
- [SDR SWAA2025071787165](https://openairdocs.org/sdr/SWAA2025071787165.md): Support Web · cracked · Jul 1, 2025 · N8696E · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING INBD. FIXED UPPER SHELF PANEL SUPPORT WEB JUST INBD. OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED SUPPORT WEB PER SRM 51-40-02.
- [SDR SWAA2025071786982](https://openairdocs.org/sdr/SWAA2025071786982.md): Skin · delaminated · Jun 30, 2025 · N8696E · Boeing 7378H4 · Trailing Edge Flaps
  > LH OTBD. AFT FLAP IS DELAMINATED LOWER INBD. CORNER. REMOVED L/H OUTBOARD AFT FLAP IAW AMM 27-51-22-000-801. REMOVED AND INSTALLED SERVICEABLE REPLACEMENT LT OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801. L/H OTBD AFT FLAP ADJUSTMENT CHECK GOOD IAW AMM 27-51-2
- [SDR SWAA2025071685829](https://openairdocs.org/sdr/SWAA2025071685829.md): Attach Angle · cracked · Jun 26, 2025 · N8696E · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND BS 663 VAPOR BARRIER ATTACH ANGLE APPROX LBL 9. REMOVED VERTICAL FASTENERS ON LT BS 663 ANGLE FROM LBL 8 TO LBL 24 IAW SRM 57-10-10-2R-5. REPAIR 5. REMOVED FUEL TANK FASTENERS FROM VAPOR BARRIER ATTACH ANGLE PER SRM 57-10-10-2R-5 REPAIR 5. 1
- [SDR SWAA2025071784794](https://openairdocs.org/sdr/SWAA2025071784794.md): Lens · missing · Jun 24, 2025 · N8696E · Boeing 7378H4 · Emergency Lighting
  > IN THE CENTER PASSENGER CABIN. THE CENTER OVERHEAD EMERGENCY EXIT LIGHT IS MISSING A LENS. INSTALLED EMERGENCY EXIT LIGHT LENS REF AMM 33-51-01.
- [SDR SWAA2025062484112](https://openairdocs.org/sdr/SWAA2025062484112.md): Flashlight · failed · Jun 21, 2025 · N8696E · Boeing 7378H4 · Emergency Equipment
  > FWD FLIGHT ATTENDANT O/B FLASHLIGHT FLASHING RED<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2025043064713](https://openairdocs.org/sdr/SWAA2025043064713.md): Battery · inoperative · Apr 27, 2025 · N8696E · Boeing 7378H4 · Emergency Equipment
  > AFT LEFT HAND OUTBOARD FA FLASHLIGHT INOP<[01] REPLACED FLASHLIGHT BATTERY AT AFT L/H OTBD POSITION REF AMM 25-64-00
- [SDR SWAA2024111458586](https://openairdocs.org/sdr/SWAA2024111458586.md): Sign · detached · Nov 11, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > EXIT ROW SIGN MID AC ON CEILING FELL OFF<[01] INSTALLED PER MM 33-51-01
- [SDR SWAA2024093042692](https://openairdocs.org/sdr/SWAA2024093042692.md): Light · inoperative · Sep 27, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > AFT LH ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BULB AT AFT LH SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2024062705984](https://openairdocs.org/sdr/SWAA2024062705984.md): Battery · inoperative · Jun 27, 2024 · N8696E · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY FLASH LIGHT INOP. REMOVED AND REPLACED AFT GALLEY FLASHLIGHT BATTERY; IAW AMM 25-64-00.
- [SDR SWAA2024062604281](https://openairdocs.org/sdr/SWAA2024062604281.md): Battery Pack · inoperative · Jun 21, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN LH EMERGENCY. LIGHT BATTERY PACK INOP AT STA 500C L/H<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 500C L/H PER AMM 33-51-06;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 500C L/H; OPS CHECK GOOD. PER AMM 33-51-06
- [SDR SWAA2024062604282](https://openairdocs.org/sdr/SWAA2024062604282.md): Battery Pack · inoperative · Jun 21, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN R/H EMERGENCY LIGHT BATTERY PACK INOP AT STA 500C R/H<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 500CR/H PER AMM 33-51-06;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 500CR/H; OPS CHECK GOOD. PER AMM 33-51-06
- [SDR SWAA2024062604284](https://openairdocs.org/sdr/SWAA2024062604284.md): Battery Pack · inoperative · Jun 21, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT BATTERY PACK IS INOP AT STA 727C L/H<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 727C L/H PER AMM 33-51-06;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 727C L/H; OPS CHECK GOOD. PER AMM 33-51-06
- [SDR SWAA2024062604283](https://openairdocs.org/sdr/SWAA2024062604283.md): Battery Pack · inoperative · Jun 21, 2024 · N8696E · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN R/H EMERGENCY LIGHT BATTERY PACK INOP AT STA 727C R/H<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 727C R/H PER AMM 33-51-06;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 727C R/H OPS CHECK GOOD. PER AMM 33-51-06
- [SDR SWAA2024062702640](https://openairdocs.org/sdr/SWAA2024062702640.md): Threshold · cracked · Jun 14, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT CORNER THRESHOLD PLATE IS CRACKED<[01] LOCATED; DRILLED AND COUNTERSUNK AFT CARGO AFT NEW CORNER THRESHOLD PLATED PER SRM 51-40-05 AND 51-40-08;[02] INSPECTED WORK ABOVE;[03] INSTALLED NEW AFT CORNER THRESHOLD. AMM 53-11-02.;[04] VERIFIED CA-3. M
- [SDR SWAA2024062702641](https://openairdocs.org/sdr/SWAA2024062702641.md): Threshold · cracked · Jun 14, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD. CORNER THRESHOLD PLATE IS CRACKED<[01] LOCATED; DRILLED AND COUNTERSINK AFT CARGO FWD NEW CORNER THRESHOLD PLATED PER SRM 51-40-05 AND 51-40-05;[02] LOCATED; DRILLED AND COUNTERSUNK AFT CARGO FWD NEW CORNER THRESHOLD PLATED PER SRM 51-40-05 AND
- [SDR SWAA2024070101277](https://openairdocs.org/sdr/SWAA2024070101277.md): Support Angle · corroded · Jun 13, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WALL SUPPORT AT STA. 997 LBL 48 HAS CORROSION AROUND FASTENER HOLES<[01] LOCATED; DRILLED; COUNTERSUNK; ALODINE AND PRIMED FASTENER HOLES ON NEW WALL SUPPORT ANGLE AT STA 997 LBL48 PER SRM 51-40-05; 51-40-08 AND 51-20-01;[02] INSPECTED AS REQUIRED; LOCATING AN
- [SDR SWAA2024070101278](https://openairdocs.org/sdr/SWAA2024070101278.md): Support · corroded · Jun 13, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WALL SUPPORT AT STA. 997 RBL 48 HAS CORROSION AROUND FASTENER HOLES<[01] LOCATED; DRILLED; COUNTERSUNK; ALODINE AND PRIMED FASTENER HOLES ON NEW WALL SUPPORT ANGLE AT STA 997 RBL48 PER SRM 51-40-05; 51-40-08 AND 51-20-01;[02] INSPECTED AS REQUIRED. CORRECTIVE
- [SDR SWAA2024062601483](https://openairdocs.org/sdr/SWAA2024062601483.md): Floor Panel · pulled · Jun 13, 2024 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242AF HAS FIBER DAMAGE<[01] R&R CABIN FLOOR PANEL 242AF IAW AMM 53-21-00;[02] UPDATE PART NUMBER;[03] C/W INSPECTION.
- [SDR SWAA2024062601484](https://openairdocs.org/sdr/SWAA2024062601484.md): Floor Panel · delaminated · Jun 13, 2024 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231YF IS DELAMINATED<[01] R&R CABIN FLOOR PANEL 231YF IAW AMM 53-21-00;[02] C/W INSPECTION.
- [SDR SWAA2024062800248](https://openairdocs.org/sdr/SWAA2024062800248.md): Floor Support · corroded · Jun 11, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN LONGITUDINAL FLOOR PANEL SUPPORT (INTERCOSTAL) HAS CORROSION AT FASTENER HOLES STA. 947+10' TO STA.947+11' AT LBL 50' AREA MARKED.<[01] LOCATED AND DRILLED NEW AFT CABIN LONGITUDINAL FLOOR PANEL SUPPORT STA 947+ 11 AT LBL 50 PER SRM 51-40-05;[02] LOC
- [SDR SWAA2024062700494](https://openairdocs.org/sdr/SWAA2024062700494.md): Floor Panel · delaminated · Jun 11, 2024 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241EF; P/N 144A5810-129 HAS DELAM AREA ON SURFACE. OK TO CIC FLOOR STRUCTURE AT PANEL 241EF; SEE STEP 2.;[03] INSTALLED NEW SERVICEABLE CABIN FLOOR PANEL 241EF PER AMM 53-21-00. INSPECTION C/W FOR WORK ACCOMPLISHED IN CORRECTIVE ACTIONS AN
- [SDR SWAA2024062799018](https://openairdocs.org/sdr/SWAA2024062799018.md): Floor Support · cracked · Jun 6, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOORBOARD SUPPORT INTERCOSTAL AT STA 540 RBL2 CRACKED. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR SWAA2024062799019](https://openairdocs.org/sdr/SWAA2024062799019.md): Floor Support · cracked · Jun 6, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOORBOARD SUPPORT INTERCOSTAL AT STA 540 LBL2 CRACKED. REMOVED DAMAGED INTERCOSTAL.;[02] R/R PASSENGER CABIN FLOORBOARD SUPPORT INTERCOSTAL AT STA 540 LBL2 IAW SRM 51-40-02.
- [SDR SWAA2024070198689](https://openairdocs.org/sdr/SWAA2024070198689.md): Floorboard · corroded · Jun 5, 2024 · N8696E · Boeing 7378H4 · Fuselage Floor Panel
  > NEED EA TO DEVIATE FROM SRM 53-70-51-2R-5 REPAIR FOR FREEZE PLUGGING FLOORBOARD HOLE.<[01] COMPLIED WITH EA 24-153-01528; WIP1 AND WIP2.;[02] 02 - INSPECTED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[03] 02 - INSPECTED PER [EA EA-GENERAL (EA ATTAC
- [SDR SWAA2024070102486](https://openairdocs.org/sdr/SWAA2024070102486.md): Floorbeam · corroded · Jun 5, 2024 · N8696E · Boeing 7378H4 · Fuselage Main, Floor Beam
  > NEED EA TO DEVIATE FROM SRM 53-70-51-2R-5 REPAIR FOR LBL 50 SHIM INSTALL DUE TO STANDOFF INTERFERENCE.<[01] COMPLIED WITH EA 24-153-01528; WIP1 AND WIP2.;[02] 02 - INSPECTED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[03] 02 - INSPECTED PER [EA EA-
- [SDR SWAA2024062800646](https://openairdocs.org/sdr/SWAA2024062800646.md): Angle · cracked · Jun 5, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE R/H AC BAY L ANGLE AT STA 663 RBL 12 RIVET HAS A CRACK EXTENDING VERTICAL TOWARDS THE CENTER FUEL TANK<REMOVED THE DAMAGED/ CRACKED R/H AC BAY VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02;[06] DRILLED UP NEW ANGLE PER 51-40-05 DRILLED NEW REPLACEMENT ANG
- [SDR SWAA2024062797261](https://openairdocs.org/sdr/SWAA2024062797261.md): Strip · corroded · Jun 2, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > THE AFT CARGO CAP STRIPS HAVE NUMEROUS AREAS OF CORROSION.<[01] REMOVED AND REPLACED DAMAGED CAP STRIPS AT AFT CARGO I/A/W AMM 25-52-10.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024062797262](https://openairdocs.org/sdr/SWAA2024062797262.md): Strip · corroded · Jun 2, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > THE FWD CARGO CAP STRIPS HAVE NUMEROUS AREAS OF CORROSION.<[01] REPLACED CAP STRIPS IN FWD CARGO IAW SRM 51-40-02 AND PER TASK CARD 'TTG8Q00S2BCS';[02] C/W INSPECTION
- [SDR SWAA2024070197265](https://openairdocs.org/sdr/SWAA2024070197265.md): Floorbeam · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM HAS UPPER SURFACE CORROSION STA 947 LBL 23-27 WL 208. MRKD<[01] MEASURED PRE BLENDING DAMAGE AND FOUND OVER 50% MATERIAL LOSS. ORIGINAL PART THICKNESS =.180?; MATERIAL LOSS IS >.090?. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A1.[17] OK TO
- [SDR SWAA2024070197266](https://openairdocs.org/sdr/SWAA2024070197266.md): Floorbeam · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT CABIN L/H I/B CREASEBEAM UPPER SURFACE HAS CORROSION STA 988 LBL 46-48 WL 208. MRKD<[01] REMOVED CORROSION STA 988 LBL 46-48; ORIGINAL MATERIAL THICKNESS IS 0.080?; MATERIAL LOSS IS 0.010?; MAX ALLOWED IS 0.008?. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-
- [SDR SWAA2024070197271](https://openairdocs.org/sdr/SWAA2024070197271.md): Floor Support · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN LONGITUDINAL FLOOR SUPPORT UPPER SURFACE CORROSION STA 949 RBL 49 WL 208. MRKD<[01] REMOVED AFT CABIN LONGITUDINAL FLOOR SUPPORT STA 949 RBL 49 WL 208 PER SRM 51-40-02;[02] BLENDED CORROSION AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1. OR
- [SDR SWAA2024070197272](https://openairdocs.org/sdr/SWAA2024070197272.md): Crease Beam · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Main, Structure
  > AFT CABIN R/H I/B CREASEBEAM UPPER SURFACE CORROSION AT STA 945-952 RBL 53-56 WL 208. MRKD<[01] BLENDED CORROSION ON CREASE BEAM(INNER CHORD) FROM STA. 945 TO STA. 952 AT RBL 54? PER SRM 51-10-02. REMOVED.043? OF MATERIAL. REMAINING THICKNESS IS.037?. DAMAGE
- [SDR SWAA2024070197273](https://openairdocs.org/sdr/SWAA2024070197273.md): Floor Support · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN LONGITUDINAL FLOOR SUPPORT UPPER SURFACE CORROSION AT FASTNER HOLES STA 957-958 RBL 49 WL 208. MRKD<[01] INTERCOSTAL FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS ON FAULT #TTG8Q00TPRV2. REFERENCE FAULT #TTG8Q00TPRV2 FOR REMOVAL AND REPLACEMENT OF INTER
- [SDR SWAA2024070197274](https://openairdocs.org/sdr/SWAA2024070197274.md): Floorbeam · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR Z-ANGLE FWD FLANGE HAS CORROSION AT STA 992 RBL 37 AND 44 WL 208. MRKD<[01] LOCATED/DRILLED FASTENER HOLES IN REPLACEMENT Z-ANGLE IAW SRM 51-40-05.;[02] 02 - INSPECTED PER SRM 51-40-02;[03] FAULT RESOLVED ON CARD #TTG8Q00TPRV5.;[04] SEE CARD# T
- [SDR SWAA2024062897210](https://openairdocs.org/sdr/SWAA2024062897210.md): Channel · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE SIDE PLATE CHANNEL FROM BS 500B TO 500C AT RBL 21 HAS SURFACE CORROSION AT VARIOUS FASTENER HOLES. BLENDED AREAS; REMOVED.002' MATERIAL, FOUND TO BE WITHIN LIMITS PER SRM 53-00-53-1A-2. FOUND FWD CARGO COMPARTMENT FLOOR
- [SDR SWAA2024062897236](https://openairdocs.org/sdr/SWAA2024062897236.md): Channel · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE SIDE PLATE CHANNEL FROM STA 500C TO 500D AT RBL 21, HAS SURFACE CORROSION AT VARIOUS FASTENER HOLES. BLENDED AREAS; REMOVED.010' MATERIAL, FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FOUND TO BE OUT OF LIMITS PER
- [SDR SWAA2024062897245](https://openairdocs.org/sdr/SWAA2024062897245.md): Channel · corroded · Jun 1, 2024 · N8696E · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE SIDE PLATE CHANNEL FROM BS 500D TO 500E AT LBL 21; HAS SURFACE CORROSION AT VARIOUS FASTENER HOLES. BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGE; TRANSITION ANGL

Next page: https://openairdocs.org/aircraft/N8696E/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 = 'N8696E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8696E/reports

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