# Service difficulty reports: N7815L

A list on [N7815L](https://openairdocs.org/aircraft/N7815L.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 · 227 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 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 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 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 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 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 SWAA2024092740908](https://openairdocs.org/sdr/SWAA2024092740908.md): Battery Pack · failed · Sep 24, 2024 · N7815L · Boeing 73776Q · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK AT R/H OVER WING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024082629575](https://openairdocs.org/sdr/SWAA2024082629575.md): Holder · out of adjust · Aug 22, 2024 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > R1 SLIDE GIRT BAR FALLS OUT OF THE HOLDER WHEN YOU OPEN THE DOOR<[01] ADJUSTED THE SLIDE CLIP GIRT DOOR HOLDER PER AMM 25-66-01 OPS CHECK GOOD
- [SDR SWAA2024082228076](https://openairdocs.org/sdr/SWAA2024082228076.md): Retainer · loose · Aug 19, 2024 · N7815L · Boeing 73776Q · Escape Slide
  > FWD SERVICE DOOR SLIDE RETAINING CLIP LOOSE.<[01] R & R?D FASTENER PER SRM 51-40-02
- [SDR SWAA2023101710687](https://openairdocs.org/sdr/SWAA2023101710687.md): Cover · broken · Oct 14, 2023 · N7815L · Boeing 73776Q · Emergency Lighting
  > RIGHT SIDE OVER WING LOWER LEVEL EXIT LIGHT COVER IS BROKEN.<[01] R&R?D RIGHT SIDE OVER WING EXIT DOOR EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01.
- [SDR SWAA2023090596938](https://openairdocs.org/sdr/SWAA2023090596938.md): Girt Bar · out of adjust · Sep 4, 2023 · N7815L · Boeing 73776Q · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR OUT OF HOLDER<[01] FOUND GIRT BAR OUT OF HOLDER; RESECURED GIRT BAR IN HOLDER REF AMM 25-66-01; SLIDE NOT AFFECTED REMAINED IN SLIDE COMPARTMENT. AIRCRAFT OK FOR SERVICE
- [SDR SWAA2023090596497](https://openairdocs.org/sdr/SWAA2023090596497.md): Blade · damaged · Sep 2, 2023 · N7815L · Boeing 73776Q · Engine (Turbine/Turboprop)
  > BIRD STRIKE #2 ENGINE; VIB 1.8 FOR 15 SECONDS. NO OTHER ABNORMAL ENGINE PARAMETERS. F/A REPORTED TURKEY SMELL IN CABIN.<[01] FOUND DAMAGE TO FAN BLADES # 11; 12 & 13 ON #2 ENG. ALSO FOUND EVIDENCE OF BIRD MATERIAL IN BOOSTER INLET. R&R FAN BLADES # 11; 12 & 13
- [SDR SWAA2023053147111](https://openairdocs.org/sdr/SWAA2023053147111.md): Rib · cracked · May 9, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB 129.50 LOWER CHORD LOCATED BTW 13.5 INCH AND 17.5 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-258231<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 210138503. DUE DATE: 19-MAY-23.;[02] PERFORMED PERMANENT REPAIR LOCAT
- [SDR SWAA2023053145335](https://openairdocs.org/sdr/SWAA2023053145335.md): Stiffener · cracked · May 4, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer Structure
  > CRACK ON STIFFENER LOCATED FRONT SPAR INSPAR RIB 129.50 AT RT HORIZONTAL STABILIZER 2023-258212<[01] REPLACED STIFFENER LOCATED ON FRONT SPAR INSPAR RIB 129.50 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 182A5305 REV: C. SEE INDIVIDUAL SIGN O
- [SDR SWAA2023053144548](https://openairdocs.org/sdr/SWAA2023053144548.md): Rib · cracked · May 3, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > CRACK ON INSPAR RIB 129.5 AND 34 INCHES FROM FRONT SPAR AT LT HORIZONTAL 2023-258208<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 210138003. DUE DATE: 2
- [SDR SWAA2023053144546](https://openairdocs.org/sdr/SWAA2023053144546.md): Rib · cracked · May 2, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > REJECT. CRACK INSPAR RIB 92.70 LOWER FLANGE AT 25 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-258206<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NO
- [SDR SWAA2023053144547](https://openairdocs.org/sdr/SWAA2023053144547.md): Rib · cracked · May 2, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > REJECT. CRACK INSPAR RIB 92.70 LOWER FLANGE AT 38 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-258207<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 17-DEC-23;[02] PERFORMED REPAIR ON INSPAR RIB 92.70 LOWER FLA
- [SDR SWAA2023053143463](https://openairdocs.org/sdr/SWAA2023053143463.md): Angle · cracked · Apr 30, 2023 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOC BS 360 ON LOWER AREA AT EQUIPMENT ELECTRONIC COMP 2023-258190<[01] REPLACED SUPPORT ANGLE LOC BS 360 ON LOWER AREA AT EQUIPMENT ELECTRONIC COMP I.A.W SOPM 20-50-01 REV 38.;[02] REPLACED SUPPORT ANGLE LOC BS 360 ON LOWER AREA AT EQUIPMEN
- [SDR SWAA2023053142509](https://openairdocs.org/sdr/SWAA2023053142509.md): Rib · cracked · Apr 27, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER 2023-258183<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM-51-40-02 AND DWG-186A1001 REV-B SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD
- [SDR SWAA2023053142510](https://openairdocs.org/sdr/SWAA2023053142510.md): Rib · cracked · Apr 27, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA 142.45 AT LT HORIZONTAL STABILIZER 2023-258184<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 142.45 AT LT HORIZONTAL STABILIZER AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV B SEE INDIVIDUAL SIGN OFF BELOW;[
- [SDR SWAA2023053130241](https://openairdocs.org/sdr/SWAA2023053130241.md): Battery Pack · inoperative · Apr 21, 2023 · N7815L · Boeing 73776Q · Emergency Lighting
  > INOP EMERGENCY LIGHT BATTERY (3EA) AT PASSENGER CABIN 2023-258105<[01] REPLACED EMERGENCY LIGHT BATTERY PACK (3EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805. AND PERFORMED INSTALLATION TEST. TEST IS OK.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CA
- [SDR SWAA2023053130242](https://openairdocs.org/sdr/SWAA2023053130242.md): Bracket · elongated · Apr 21, 2023 · N7815L · Boeing 73776Q · Leading Edge Devices
  > ELONGATED HOLE SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING 2023-258140<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING IAW B737-700 SRM 52-10-02 ITEM 9.;[02] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT
- [SDR SWAA2023053129767](https://openairdocs.org/sdr/SWAA2023053129767.md): Bracket · cracked · Apr 20, 2023 · N7815L · Boeing 73776Q · Leading Edge Devices
  > CRACK SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING 2023-258133<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING IAW B737-700 SRM 51-40-02;[02] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING IAW B737
- [SDR SWAA2023053129768](https://openairdocs.org/sdr/SWAA2023053129768.md): Rib · cracked · Apr 20, 2023 · N7815L · Boeing 73776Q · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA198.23 RT HORIZONTAL STAB 2023-258134<[01] REPLACED LEADING EDGE RIB LOCATED LE STA198.23 RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV B SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFI
- [SDR SWAA2023053129210](https://openairdocs.org/sdr/SWAA2023053129210.md): Angle · cracked · Apr 19, 2023 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 727 RBL 3 FWD PARTITION AT AFT CARGO COMPARTMENT 2023-258112<[01] REMOVED ANGLE DUE TO CRACK LOCATED BS 727 RBL 3 FWD PARTITION AT AFT CARGO COMPARTMENT; PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND ADDITIONAL DAMAGE AND
- [SDR SWAA2023053129209](https://openairdocs.org/sdr/SWAA2023053129209.md): Plate · cracked · Apr 19, 2023 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACK ON SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2023-258109<[01] REPLACED SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-146A0081 REV: A SEE IND
- [SDR SWAA2023053129208](https://openairdocs.org/sdr/SWAA2023053129208.md): Angle · cracked · Apr 19, 2023 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 907 PLUS 11 INCHES BTW STR 23R TO STR 25R AT AFT CARGO COMPARTMENT 2023-258108<[01] REPLACED SUPPORT ANGLE LOCATED BS 907 BTW STR 23R TO STR 25R AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 147A7
- [SDR SWAA2023053129211](https://openairdocs.org/sdr/SWAA2023053129211.md): Web · corroded · Apr 19, 2023 · N7815L · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R RBL 22 WL 156 AT AFT CARGO COMPARTMENT 2023-258113<[01] REPLACED WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R RBL 22 WL 156 AT AFT CARGO COMPARTMENT AND FASTENERS IAW B77-700 SRM 51-10-02 ITEM

Next page: https://openairdocs.org/aircraft/N7815L/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 = 'N7815L' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7815L/reports

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