# Service difficulty reports: Boeing 737-76Q

A list on [Boeing 737-76Q](https://openairdocs.org/model/boeing-737-76q.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 33 · 1,627 reports

- [SDR SWAA2026042890560](https://openairdocs.org/sdr/SWAA2026042890560.md): Web · cracked · Apr 18, 2026 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > APB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-01061-DTI..
- [SDR SWAA2025122955746](https://openairdocs.org/sdr/SWAA2025122955746.md): Regulator · low pressure · Dec 26, 2025 · N565WN · Boeing 73776Q · Pneumatic Distribution System
  > AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. A
- [SDR SWAA2025122956227](https://openairdocs.org/sdr/SWAA2025122956227.md): Regulator · low pressure · Dec 26, 2025 · N565WN · Boeing 73776Q · Pneumatic Distribution System
  > AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PE
- [SDR SWAA2025122956228](https://openairdocs.org/sdr/SWAA2025122956228.md): Valve · low pressure · Dec 26, 2025 · N565WN · Boeing 73776Q · Pneumatic Distribution System
  > AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00.
- [SDR SWAA2025122956229](https://openairdocs.org/sdr/SWAA2025122956229.md): Valve · low pressure · Dec 26, 2025 · N565WN · Boeing 73776Q · Pneumatic Distribution System
  > AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11 NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.5 PSID NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. P
- [SDR SWAA2025121651775](https://openairdocs.org/sdr/SWAA2025121651775.md): Screw · missing · Dec 12, 2025 · N565WN · Boeing 73776Q · Emergency Exits
  > LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING SCREW IAW AMM 12-25-22.
- [SDR SWAA2025090912957](https://openairdocs.org/sdr/SWAA2025090912957.md): Fseu · faulted · Sep 8, 2025 · N565WN · Boeing 73776Q · Trailing Edge Flap Control System
  > TRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. REPLACED FSEU IAW AMM 27-51-01. OPS CHECKED GOOD.
- [SDR SWAA2025090210292](https://openairdocs.org/sdr/SWAA2025090210292.md): Sensor · faulted · Sep 1, 2025 · N565WN · Boeing 73776Q · Trailing Edge Flap Control System
  > AFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FLAP SWITCH PER QRH. THE LANDING WAS NORMAL AND UNEVENTFUL. R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01.
- [SDR SWAA2025082606374](https://openairdocs.org/sdr/SWAA2025082606374.md): Cap · missing · Aug 20, 2025 · N7815L · Boeing 73776Q · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HANDLE HAS MISSING STUD CAP. INSTALLED STUD CAP IAW AMM 52-31-14.
- [SDR SWAA2025082206375](https://openairdocs.org/sdr/SWAA2025082206375.md): Handle · missing · Aug 20, 2025 · N7815L · Boeing 73776Q · Cargo/Baggage Doors
  > AFT CARGO DOOR HANDLE HAS MISSING STUD CAP<[01] REMOVED AND REPLACED AFT CARGO DOOR HANDLE STUD CAP REFERENCE AMM52-31-14.
- [SDR SWAA2025081804438](https://openairdocs.org/sdr/SWAA2025081804438.md): Flap System · faulted · Aug 14, 2025 · N565WN · Boeing 73776Q · Trailing Edge Flap Control System
  > AS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELECTED F5, SAME RESULT. RETURNED FLAP HANDLE TO ZERO CHECKED CIRCUIT BREAKERS, ALL IN, AND EXECUT
- [SDR SWAA2025081299599](https://openairdocs.org/sdr/SWAA2025081299599.md): Girt Bar · damaged · Aug 8, 2025 · N7815L · Boeing 73776Q · Emergency Equipment
  > FWD ENTRY DOOR GURT BAR HOOK HAS MISSING RIVET. INSTALLED NEW RIVET IN FWD ENTRY GURT BAR HOOK REF SIP
- [SDR SWAA2025062785458](https://openairdocs.org/sdr/SWAA2025062785458.md): Skirt · out of position · Jun 25, 2025 · N565WN · Boeing 73776Q · Escape Slide
  > AFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06.
- [SDR SWAA2025060276185](https://openairdocs.org/sdr/SWAA2025060276185.md): Girt Bar · loose · May 28, 2025 · N7815L · Boeing 73776Q · Emergency Equipment
  > R1 DOOR GIRT BAR LOOSE <[01]. RE-SECURED R1 DOOR GIRT BAR RETAINER CLIPS PER AMM 25-66-01. OPS CHK GOOD.
- [SDR SWAA2025051971778](https://openairdocs.org/sdr/SWAA2025051971778.md): Slide · loose · May 15, 2025 · N7815L · Boeing 73776Q · Escape Slide
  > R1 SLIDE CAME LOOSE. REINSTALLED SLIDE PER MT#25-66-01.
- [SDR SWAA2025050667536](https://openairdocs.org/sdr/SWAA2025050667536.md): Sign · inoperative · May 4, 2025 · N565WN · Boeing 73776Q · Emergency Lighting
  > CREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01.
- [SDR SWAA2025050622175](https://openairdocs.org/sdr/SWAA2025050622175.md): Battery Pack · inoperative · Apr 7, 2025 · N7815L · Boeing 73776Q · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY BATTERY PACK M2335 IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025050608576](https://openairdocs.org/sdr/SWAA2025050608576.md): Strip · cracked · Mar 23, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > FWD CARGO BAY SIDEWALL PNL 122AW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE7;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.
- [SDR SWAA2025050615939](https://openairdocs.org/sdr/SWAA2025050615939.md): Strip · cracked · Mar 23, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > FWD CARGO BAY SIDEWALL PNL 122EW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE1;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2025050615928](https://openairdocs.org/sdr/SWAA2025050615928.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02;[02] OK TO INSTALL;[03] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727D S-6L PER DWG 146A1111 AND SRM 51-40-02.
- [SDR SWAA2025050615929](https://openairdocs.org/sdr/SWAA2025050615929.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02;[02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L PER DWG 146A1103 REV D AND SRM 51-40-02.
- [SDR SWAA2025050615930](https://openairdocs.org/sdr/SWAA2025050615930.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727D S-4R. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111 AND SRM 51-40-02.
- [SDR SWAA2025050615931](https://openairdocs.org/sdr/SWAA2025050615931.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727A S-5R. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1101 REV AND SRM 51-40-02.
- [SDR SWAA2025050606638](https://openairdocs.org/sdr/SWAA2025050606638.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727B S-5R. MARKED. REMOVED AND REPLACED NEW STRINGER CLIP BS727B S-5R PER DWG 146A1103 REV D AND SRM 51-40-02. CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.
- [SDR SWAA2025040906636](https://openairdocs.org/sdr/SWAA2025040906636.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED <[01]. REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02; [02] OK TO INSTALL; [03] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727D S-6L PER DWG 146A1111 AND SRM 51-40-02.
- [SDR SWAA2025040906637](https://openairdocs.org/sdr/SWAA2025040906637.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED <[01]. REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L PER DWG 146A1103 REV D AND SRM 51-40-02.
- [SDR SWAA2025040906639](https://openairdocs.org/sdr/SWAA2025040906639.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED <[01]. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111 AND SRM 51-40-02.
- [SDR SWAA2025040906640](https://openairdocs.org/sdr/SWAA2025040906640.md): Stringer Clip · cracked · Mar 18, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727A S-5R. MARKED <[01]. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1101 REV AND SRM 51-40-02.
- [SDR SWAA2025050606464](https://openairdocs.org/sdr/SWAA2025050606464.md): Skin · corroded · Mar 17, 2025 · N7815L · Boeing 73776Q · Vertical Stabilizer, Plate/Skin
  > CORROSION ON UPPER FUSELAGE SKIN UNDER VERTICAL STAB LBL12 TO RBL12 BS1016 - BS1078 WL308.5. MARKED<[01] UPDATED TABLE; COMPLETED STEP 9.;[02] ' AS PER EA 25-153-00791; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS
- [SDR SWAA2025040906466](https://openairdocs.org/sdr/SWAA2025040906466.md): Angle · corroded · Mar 17, 2025 · N7815L · Boeing 73776Q · Vertical Stabilizer Miscellaneous Structure
  > CORROSION ON ANGLE UNDER VERTICAL STAB BS1036 LBL2 WL308.5. MARKED <[01]. ADDED DIMENSIONS TO STEP 2.
- [SDR SWAA2025050615901](https://openairdocs.org/sdr/SWAA2025050615901.md): Plate · cracked · Mar 15, 2025 · N7815L · Boeing 73776Q · Wing Miscellaneous Structure
  > WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4. VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
- [SDR SWAA2025040905686](https://openairdocs.org/sdr/SWAA2025040905686.md): Plate · cracked · Mar 15, 2025 · N7815L · Boeing 73776Q · Trailing Edge Flaps
  > WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED <[01]. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4.; [02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
- [SDR SWAA2025050605541](https://openairdocs.org/sdr/SWAA2025050605541.md): Scuff Plate · cracked · Mar 14, 2025 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > ACB FWD CORNER SCUFF PLATE CRACKED(MARKED)<[01] 04 - REPAIRED PER [SRM 53-60-15-2R-1-A00967 (REPAIR 1 - AFT CARGO DOOR SURROUND STRUCTURE - PERMANENT)]
- [SDR SWAA2025050639172](https://openairdocs.org/sdr/SWAA2025050639172.md): Attach Fitting · corroded · Mar 13, 2025 · N7815L · Boeing 73776Q · Wing, Attach Fittings
  > CORROSION ON LEFT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING STRAP ATTACHMENT POINT - IFSS 121.<[01] REPAIRED CORROSION ON LEFT WING FRONT SPAR BOOST PUMP AT UPPER BONDING STRAP ATTACH POINT AT IFSS121 IAW WITH SWA EA 25-157-00744 (AD- N7815L - ATS(PAE) -
- [SDR SWAA2025050615880](https://openairdocs.org/sdr/SWAA2025050615880.md): Pressure Deck · cracked · Mar 13, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Structure
  > CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED)<[01] REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS 663 RBL 30 TO RBL 60 PER B-737-700 SRM 53-40-51-2R-2 REPAIR 2 STEP 4 A-N.;[02] COMPLETE;[03] FAULT
- [SDR SWAA2025040905218](https://openairdocs.org/sdr/SWAA2025040905218.md): Pressure Deck · cracked · Mar 13, 2025 · N7815L · Boeing 73776Q · Fuselage Main, Structure
  > CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED) <[01]. REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS 663 RBL 30 TO RBL 60 PER B-737-700 SRM 53-40-51-2R-2 REPAIR 2 STEP 4 A-N.; [02] COMPLETE; [03] F
- [SDR SWAA2025050604854](https://openairdocs.org/sdr/SWAA2025050604854.md): Strut · cracked · Mar 12, 2025 · N7815L · Boeing 73776Q · Landing Gear Door Retract Section
  > L/H MLG GEAR STRUT DOOR IS CRACKED<[01] UPDATED STEPS 1;2 FOR REMOVAL L/H MLG SHOCK STRUT DOORS;[02] COMPLETED STEPS 2;4;[03] COMPLETED STEP 1 INSTALL L/H MLG SHOCK STRUT DOORS.;[04] REMOVED; REPAIRED; REINSTALLED; ADJUSTED AND PERFORMED GOOD INSTALLATION TEST
- [SDR SWAA2025022699482](https://openairdocs.org/sdr/SWAA2025022699482.md): Lens · missing · Feb 24, 2025 · N565WN · Boeing 73776Q · Emergency Lighting
  > L/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIP
- [SDR SWAA2025022699061](https://openairdocs.org/sdr/SWAA2025022699061.md): Control Unit · malfunctioned · Feb 23, 2025 · N7815L · Boeing 73776Q · Overheat Detection
  > INTERMITTANT RIGHT WING/BODY OVERHEAT LIGHT ON APPROACH LIGHT EXTINGUISHED SHORT AFTER ILLUMINATION<[01] PERFORMED COMPARTMENT OVERHEAT DETECTION CONTROL UNIT BITE CHECK PER AMM 26-18-00 AND WING BODY OVERHEAT TEST PER AMM 26-18-01; FAULT CLEARED AND OPS CHECK
- [SDR SWAA2025012789283](https://openairdocs.org/sdr/SWAA2025012789283.md): Shroud · misinstalled · Jan 24, 2025 · N565WN · Boeing 73776Q · Escape Slide
  > FWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01/401-MT 725-61-06.;[03] VERIFIED CORRECTIVE ACTI
- [SDR SWAA2025012788590](https://openairdocs.org/sdr/SWAA2025012788590.md): Light · inoperative · Jan 22, 2025 · N565WN · Boeing 73776Q · Emergency Lighting
  > EMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025012388436](https://openairdocs.org/sdr/SWAA2025012388436.md): Elec Connector · disconnected · Jan 22, 2025 · N565WN · Boeing 73776Q · Light System Wiring
  > EMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGHT L1419 PER SWPM 20-63-02. PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-00-710-801;[02] VERIFIED CO
- [SDR SWAA2025012385910](https://openairdocs.org/sdr/SWAA2025012385910.md): Seat Track · cracked · Jan 14, 2025 · N565WN · Boeing 73776Q · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025012884184](https://openairdocs.org/sdr/SWAA2025012884184.md): Track · cracked · Jan 8, 2025 · N565WN · Boeing 73776Q · Stabilizer Control System
  > RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2025012283949](https://openairdocs.org/sdr/SWAA2025012283949.md): Scuff Plate · cracked · Jan 7, 2025 · N565WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > FCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2025012283947](https://openairdocs.org/sdr/SWAA2025012283947.md): Scuff Plate · cracked · Jan 7, 2025 · N565WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > ACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIED
- [SDR SWAA2025012283948](https://openairdocs.org/sdr/SWAA2025012283948.md): Scuff Plate · cracked · Jan 7, 2025 · N565WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > ACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIED
- [SDR SWAA2025012283447](https://openairdocs.org/sdr/SWAA2025012283447.md): Floorbeam · cracked · Jan 6, 2025 · N565WN · Boeing 73776Q · Fuselage Main, Floor Beam
  > BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025012283452](https://openairdocs.org/sdr/SWAA2025012283452.md): Floorbeam · cracked · Jan 6, 2025 · N565WN · Boeing 73776Q · Fuselage Main, Floor Beam
  > BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B<BR>INSTALLED PANEL 231UF IAW AMM 53-21-00-400-801;[02] CORRECTIVE ACTION COMPLET
- [SDR SWAA2025012083130](https://openairdocs.org/sdr/SWAA2025012083130.md): Floor Panel · pulled · Jan 5, 2025 · N565WN · Boeing 73776Q · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0007.;[02] VER

Next page: https://openairdocs.org/model/boeing-737-76q/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 aircraft_model_key = '73776Q'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-76q/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.