# Service difficulty reports: N7825A

A list on [N7825A](https://openairdocs.org/aircraft/N7825A.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 4 · 196 reports

- [SDR SWAA2026101272071](https://openairdocs.org/sdr/SWAA2026101272071.md): Tray Table · broken · Oct 7, 2026 · N7825A · Boeing 7377CT · Passenger Compartment Equipment
  > PASSENGER SEAT TRAY TABLE DAMAGED. REPLACED MISSING SCREW IAW AMM 25-22-00.
- [SDR SWAA2026090803429](https://openairdocs.org/sdr/SWAA2026090803429.md): Engine · shutdown · Sep 3, 2026 · N7825A · Boeing 7377CT · Engine (Turbine/Turboprop)
  > NR 2 ENGINE SHUTDOWN ON TAXI OUT, RESTARTED WITH NO FURTHER INCIDENT. CHECKED IDG OIL LEVEL, CHECKED GOOD. CHECKED NR 2 SPAR VALVE OPERATION, CHECKED GOOD IAW MM 28-22-00. STARTED NR 2 ENGINE, OPS CHECKED GOOD IAW MM 71-00-00. PERFORMED EEC BITE AND NO FAU
- [SDR SWAA2026043093048](https://openairdocs.org/sdr/SWAA2026043093048.md): Metering Valve · failed · Apr 26, 2026 · N7825A · Boeing 7377CT · Landing Gear Brake System
  > LINED UP AIRCRAFT ON 27R, ENGINES STABILIZED AT 40% N1, RELEASE BRAKES AND ACFT IMMEDIATELY PULLS HARD RIGHT 30-35. ABORTED TAKE OFF AND TAXIED BACK TO GATE. GROUND SPEED LESS THAN 20 KNOTS. F/O APPLIED FULL LEFT RUDDER CAPT USED LEFT TILLER INPUTS TO KEEP A
- [SDR SWAA2025122253871](https://openairdocs.org/sdr/SWAA2025122253871.md): Clamp · out of adjust · Dec 19, 2025 · N7825A · Boeing 7377CT · Emergency Equipment
  > FWD SERVICE DOOR HAS A LOOSE RETENTION GIRT BAR CLAMP. ADJUSTED FWD SERVICE DOOR GIRT BAR CLAMPS PER SIP.
- [SDR SWAA2025121752557](https://openairdocs.org/sdr/SWAA2025121752557.md): Screw · missing · Dec 14, 2025 · N7825A · Boeing 7377CT · Escape Slide
  > RIGHT FORWARD SERVICE DOOR EMERGENCY EVAC SLIDE COVER LEFT SIDE SCREW IS MISSING. INSTALLED NEW FASTENER @FWD SERVICE DOOR SLIDE CONTAINER IAW AMM 20-50-11.
- [SDR SWAA2025100319191](https://openairdocs.org/sdr/SWAA2025100319191.md): Fuel Sys · leaking · Sep 29, 2025 · N7825A · Boeing 7377CT · Fuel Storage
  > SUSPECTED FUEL LEAK FROM NO.1 ENGINE SIDE. NEEDED TO CROSSFEED TWICE DUE TO 400 LB. IMBALANCE. NOTED FUEL FLOW NR 1 SIDE HIGHER THAN NR 2 SIDE BY AS MUCH AS 200 LBS PER HOUR AT CRUISE. POSSIBLE FLUID ON FLAP ON NR 1 SIDE. FUEL BURN STL-BWI 400 LBS GREATER BETW
- [SDR SWAA2025040720989](https://openairdocs.org/sdr/SWAA2025040720989.md): Air Data Module · failed · Apr 2, 2025 · N7825A · Boeing 7377CT · Air Data Computer
  > IAS DISAGREE ON BOTH PFDS - CAPT SIDE UNRELIABLE. LOST AIRSPEED / ALTITUDE / EECS ON ALTN / SPEED TRIM FAIL.<[01] R&R FO?S AIR DATA MODULE IAW AMM 34-21-04;[02] R&R FO?S AIR DATA MODULE IAW AMM 34-21-04<BR>A/C RECERTIFIED TO CAT III STATUS PER MT 734-00-03<BR>
- [SDR SWAA2025022498763](https://openairdocs.org/sdr/SWAA2025022498763.md): O-Ring · leaking · Feb 20, 2025 · N7825A · Boeing 7377CT · Hydraulic System, Main
  > SUSPECTED HYDRAULIC LEAK IN MAIN WHEEL WELL. REMOVED AND REPLACED O-RING AT BOTTOM OF ALT. BRAKE SELECTOR VALVE REF AMM 32-41-93
- [SDR SWAA2025021294982](https://openairdocs.org/sdr/SWAA2025021294982.md): Battery Pack · inoperative · Feb 11, 2025 · N7825A · Boeing 7377CT · Emergency Lighting
  > ALL EMERGENCY LIGHTS RELATED TO BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT; AND PERFORMED GOOD INSTALLATION TEST OF M2335 BATTERY PACK AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021389623](https://openairdocs.org/sdr/SWAA2025021389623.md): Threshold Web · corroded · Jan 25, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > .MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+6 TO BS460+13 RBL30;WL156<[01] FCB DOOR CUTOUT SURROUND THRESHOLD REPAIR BY REPLACEMENT PER 51-10-02-0G-0. RECIVED NEW WEB P/N 654A0003-58 LOT. 1588648-1<BR>LOCATED AND DRLLED NEW WEB IA
- [SDR SWAA2025021389624](https://openairdocs.org/sdr/SWAA2025021389624.md): Threshold · corroded · Jan 25, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON ACB DOOR CUTOUT SURROUND THRESHOLD BS794.3 TO BS827+3 RBL30 WL156.<[01] UPDATED STEP 3;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[03] VERIF
- [SDR SWAA2025021388732](https://openairdocs.org/sdr/SWAA2025021388732.md): Seat Track · corroded · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 45.5 BS616+10; BS616+13; BS616+14; BS639+15; BS663+15; BS663+18; WL 208 (MARKED)<[01] CERTIFY ACTION #2;[02] UPDATED MEASUREMENT TABLE;[03] PARTIAL UPDATE STEP #4;[04] REMOVED AND REMPLACED SEAT TRACK FROM RBL 45 BS 540 TO BS 727B W
- [SDR SWAA2025021388731](https://openairdocs.org/sdr/SWAA2025021388731.md): Seat Track · corroded · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 45.5 BS540+1.5; BS540+8; BS540+11.5; BS540+19; BS559+7; BS559+15; BS578+13; BS597+4; BS597+8.5; BS597+12; BS597+13 (MARKED)<[01] SEAT TRACK AT BS 540-727B RBL45.5 IS OUT OF LIMITS AT BS 663+15. TO BE REPLACED ON TTG8Q00YA3DT.;[02] V
- [SDR SWAA2025021388733](https://openairdocs.org/sdr/SWAA2025021388733.md): Seat Track · corroded · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 45.5 BS706+4; BS706+5.5; BS706+7; BS706+17.5; BS727+13; BS727+17.5; BS727A+6.5; BS727A+8.5 WL 208 (MARKED<[01] SEAT TRACK AT BS 540-727B; RBL 45 IS OUT OF LIMITS AT BS 663+15. TO BE REPLACED ON TTG8Q00YA3DT;[02] VERIFIED CORRECTIVE
- [SDR SWAA2025021288726](https://openairdocs.org/sdr/SWAA2025021288726.md): Floor Panel · pulled · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0127.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025021088724](https://openairdocs.org/sdr/SWAA2025021088724.md): Floor Panel · pulled · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF HAS BEEN REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025021088727](https://openairdocs.org/sdr/SWAA2025021088727.md): Floor Panel · pulled · Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 04 - REPAIRED PULLED STRANDS ON UPPER SURFACE PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025021388720](https://openairdocs.org/sdr/SWAA2025021388720.md): Scuff Plate · cracked · Jan 22, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FWD CORNER SCUFFPLATE IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-60-15-2R-1;[02] REPAIRED AFT CARGO COMPARTMENT FWD CORNER SCUFFPLATE PER SRM 53-60-15-2R-1. APPLIED CHEMICAL CONVERSION COATING PER SOPM 20-43-03; APPLIED PROTECTIVE
- [SDR SWAA2025021387665](https://openairdocs.org/sdr/SWAA2025021387665.md): Panel · debonded · Jan 19, 2025 · N7825A · Boeing 7377CT · Wing, Plate/Skin
  > RIGHT WING L/E PANEL 621DB HAS DISBONDS AT I/B FWD CORNER AND FWD PANEL CUTOUT CORNERS<[01] RIGHT WING L/E PANEL 621DB WAS REPAIRED IAW SRM 51-70-05-2R-6;[02] JOB COMPLETE.
- [SDR SWAA2024102852089](https://openairdocs.org/sdr/SWAA2024102852089.md): Battery Pack · failed · Oct 23, 2024 · N7825A · Boeing 7377CT · Emergency Lighting
  > L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024102852088](https://openairdocs.org/sdr/SWAA2024102852088.md): Battery Pack · failed · Oct 23, 2024 · N7825A · Boeing 7377CT · Emergency Lighting
  > R/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024070308105](https://openairdocs.org/sdr/SWAA2024070308105.md): Doubler · cracked · Jul 2, 2024 · N7825A · Boeing 7377CT · Fuselage Main, Plate/Skin
  > EXTERNAL POWER DOOR DOUBLER CUTOUT CRACKED<[01] REPAIRED DAMAGED PER SRM 53-10-15-2R-4;[02] VERIFIED REPAIRED DAMAGED PER SRM 53-10-15-2R-4
- [SDR SWAA2024070106886](https://openairdocs.org/sdr/SWAA2024070106886.md): Doubler · cracked · Jun 27, 2024 · N7825A · Boeing 7377CT · Accessory Compartment Doors
  > EXTERNAL POWER DOOR DOUBLER CUTOUT CRACKED<[01] COMPLIED WITH EA 24-153-01763
- [SDR SWAA2024062103450](https://openairdocs.org/sdr/SWAA2024062103450.md): Handle · loose · Jun 20, 2024 · N7825A · Boeing 7377CT · Emergency Exits
  > LEFT EMERGENCY HATCH ASSIST HANDLE SURROUND NOT SECURE<[01] 01 - RESECURED LEFT EMERGENCY HATCH ASSIST HANDLE SURROUND PER [AMM 52-22-51-400-801-NG (EMERGENCY EXIT DOOR LINING INSTALLATION - PERMANENT)]
- [SDR SWAA2023112724727](https://openairdocs.org/sdr/SWAA2023112724727.md): Slide · out of limits · Nov 25, 2023 · N7825A · Boeing 7377CT · Escape Slide
  > AFT LEFT EMERGENCY ESCAPE SLIDE PRESSURE GAUGE BELOW LIMITS.<[01] REMOVED AND REPLACED AFT ENTRY DOOR ESCAPE SLIDE REF MM 25-66-01.
- [SDR SWAA2023101309589](https://openairdocs.org/sdr/SWAA2023101309589.md): Panel · delaminated · Oct 11, 2023 · N7825A · Boeing 7377CT · Engine (Turbine/Turboprop)
  > #2 ENGINE; AFT ACOUSTICAL PANEL ABOVE THE 3 OCLOCK STRUT HAS DELAMINATED SKIN WITH EXPOSED CORE<[01] R&R?D #2 ENG; AFT ACOUSTICAL PANEL LOCATED ABOVE 3 O?CLOCK STRUT REF AMM 72-23-02.
- [SDR SWAA2023021494067](https://openairdocs.org/sdr/SWAA2023021494067.md): Support Angle · cracked · Jan 22, 2023 · N7825A · Boeing 7377CT · Wing Spar
  > CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR WEB BOOST PUMP IFSS 120 AT LT WING 2023-38078<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30 S/N: 0000293 DUE DATE: 12-OCT-2023.;[02] TOOL USED: POWER PACK P/N FMK0003223 S/N PE0412/63335 DUE DATE: 26-JAN-23. MULTIMETE
- [SDR SWAA2023021491846](https://openairdocs.org/sdr/SWAA2023021491846.md): Panel · elongated · Jan 15, 2023 · N7825A · Boeing 7377CT · Horizontal Stabilizer Structure
  > ELONGATED HOLE LOC. BTW STAB STA133.15 TO STA 151.15 AT L/H HORIZONTAL STABILIZER LEADING EDGE PANEL 2023-38061<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] PERFORMED PERMANENT REPAIR ON L/H HORIZONTAL STABILIZ
- [SDR SWAA2023021491842](https://openairdocs.org/sdr/SWAA2023021491842.md): Bracket · cracked · Jan 15, 2023 · N7825A · Boeing 7377CT · Wing, Center Box
  > CRACK BODY STATION 540 LBL 19 BRACKET AT AIR CONDITIONING BAY 2023-38044<[01] REPLACED BRACKET LOCATED AT BODY STATION 540 LBL 19 AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SINGOFFS BELOW.;[02] REPLACED BRACKET LOCATED AT BODY STATION 540 LB
- [SDR SWAA2023021491843](https://openairdocs.org/sdr/SWAA2023021491843.md): Angle · cracked · Jan 15, 2023 · N7825A · Boeing 7377CT · Wing, Center Box
  > CRACK BODY STA 663.75 ANGLE RBL 19 AT AIR CONDITIONING BAY 2023-38046<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[02] REPLACED BODY STA 663.75 ANGLE RBL 19 AT AIR CONDITIONING BAY IAW B-737-700 SRM 51-40-02 AND
- [SDR SWAA2023021491844](https://openairdocs.org/sdr/SWAA2023021491844.md): Angle · cracked · Jan 15, 2023 · N7825A · Boeing 7377CT · Wing, Center Box
  > CRACK BODY STA 663.75 ANGLE LBL 20 AT AIR CONDITIONING BAY 2023-38045<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[03] R
- [SDR SWAA2023021391845](https://openairdocs.org/sdr/SWAA2023021391845.md): Angle · cracked · Jan 15, 2023 · N7825A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK BODY STA 663.75 ANGLE RBL 43 AT AIR CONDITIONING BAY 2023-38047<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00H93R9;[02] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00H93R9
- [SDR SWAA2023021491563](https://openairdocs.org/sdr/SWAA2023021491563.md): Web · corroded · Jan 13, 2023 · N7825A · Boeing 7377CT · Leading Edge Devices
  > CORROSION FRONT SPAR ON INDICATOR FUEL TANK WEB AT RT WING 2023-38015<[01] REPLACED REFUEL PANEL P15 IAW B737-700 AMM 28-21-00-000-801; AMM 28-41-61-000-801; AMM 28-21-00-400-801 AND 28-41-61-400-801; TEST IS OK; TOOL USED: MILLIOHMETTER; P/N: M1 MILLIOHM METE
- [SDR SWAA2023021391366](https://openairdocs.org/sdr/SWAA2023021391366.md): Strip · broken · Jan 13, 2023 · N7825A · Boeing 7377CT · Emergency Lighting
  > BROKEN CARPET PHOTOLUMINESCENTS STRIPS (10EA) AT PASSENGER CABIN (10 EA) 2023-38003<[01] REPLACED CARPET PHOTOLUMINESCENTS STRIPS (10EA) AT PASSENGER CABIN (10 EA IAW B737-700 AMM 33-51-15-960-801;[02] CORRECTIVE ACTION CERTIFIED
- [SDR SWAA2023021491241](https://openairdocs.org/sdr/SWAA2023021491241.md): Track · cracked · Jan 12, 2023 · N7825A · Boeing 7377CT · Fuselage Internal Mounting Structure
  > CRACK TRACK RBBL 13.80 LOCATED BS 727E AFT CARGO COMPARTMENT 2023-37981<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 11-APR-23;[02] PERFORMED REPAIR ON CARGO TRACK RBBL 13.80 LOCATED BS 727D TO BS 767 AT AFT CARGO COMPARTMENT. I
- [SDR SWAA2023021491003](https://openairdocs.org/sdr/SWAA2023021491003.md): Support Angle · cracked · Jan 12, 2023 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AFT POSITION RBL 4 AT AFT CARGO COMPARTMENT 2023-37978<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AFT POSITION RBL 4 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02. SING INDIVIDUAL SEE OFF
- [SDR SWAA2023021491001](https://openairdocs.org/sdr/SWAA2023021491001.md): Support · corroded · Jan 12, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 787 TO BS 727B LBL 21 WL 156 AFT CARGO COMPARTMENT 2023-37979<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221861811;CAL DUE DATE: 08-NOV-23;[02] REPLACED SUPPORT ZEE AND FASTENER LOC ON BS727 TO BS847 LBL 21
- [SDR SWAA2023021490852](https://openairdocs.org/sdr/SWAA2023021490852.md): Support Angle · cracked · Jan 11, 2023 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 807 RBL 21 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2023-37954<[01] REPLACED ANGLE - SUPPORT LOCATED BS 807 RBL 21 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 51-40-02 AND DWG 146A8340 SH 18 REV-RII ITEM;[
- [SDR SWAA2023021490854](https://openairdocs.org/sdr/SWAA2023021490854.md): Stringer · cracked · Jan 11, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 27R BS 540 FWD CARGO COMPARTMENT 2023-37966<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 130066401; DUE DATE: 21-SEP-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CON
- [SDR SWAA2023021490851](https://openairdocs.org/sdr/SWAA2023021490851.md): Rib · cracked · Jan 11, 2023 · N7825A · Boeing 7377CT · Horizontal Stabilizer Structure
  > CRACK LEADING EDGE RIB LOCATED L/E STA. 78.29 AT LT HORIZONTAL STABILIZER 2023-37953<[01] REPLACED RIB LOCATED L/E STA. 78.29 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 186A1001 RE:B; SEE INDIVIDUAL SIGNOFF BELOW.;[
- [SDR SWAA2023021490075](https://openairdocs.org/sdr/SWAA2023021490075.md): Rib · cracked · Jan 10, 2023 · N7825A · Boeing 7377CT · Horizontal Stabilizer Structure
  > CRACK ON UPPER CHORD OF INSPAR RIB 120.30 FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-37915<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE
- [SDR SWAA2023021490076](https://openairdocs.org/sdr/SWAA2023021490076.md): Rib · cracked · Jan 10, 2023 · N7825A · Boeing 7377CT · Horizontal Stabilizer Structure
  > CRACK LOWER CHORD OF INSPAR RIB STAB STA 120.30 FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-37916<[01] 'REFERT TO FAULT TTG8Q00H5JYF WHERE EA 23-155-00202 WAS ADDED AS A SUBTASK ';[02] REFERT TO FAULT TTG8Q00H5JYF WHERE EA 23-155-00202 WAS ADDED AS A SUBTASK;
- [SDR SWAA2023021490470](https://openairdocs.org/sdr/SWAA2023021490470.md): Rib · cracked · Jan 10, 2023 · N7825A · Boeing 7377CT · Horizontal Stabilizer Structure
  > CRACK LEADING EDGE RIB LOCATED LE STA 151.75 RT HORIZONTAL STAB 2023-37939<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 151.75 RT HORIZONTAL STAB IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 186A1001 SHEET 1 REV: B; SEE INDIVIDUAL SIGN OFF BELOW
- [SDR SWAA2023021490468](https://openairdocs.org/sdr/SWAA2023021490468.md): Actuator · cracked · Jan 10, 2023 · N7825A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK FUEL FLOAT ACTUATOR ON VALVE ACTUATOR VENT BTW RIB 21 AND RIB 22 AT RT WING 2023-37926<[01] REPLACED FLOAT ACTUATOR ON VALVE ACTUATOR VENT BTW RIB 21 AND RIB 22 AT RT WING IAW B737-700 AMM 28-13-11-400-801 SEE INDIVIDUAL SING OFF BELOW;[02] TASK COMPLETE
- [SDR SWAA2023021490069](https://openairdocs.org/sdr/SWAA2023021490069.md): Bracket · cracked · Jan 9, 2023 · N7825A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK BILGE AREA BRACKET LOC BS 400 AND LBL 21.80 AT FWD CARGO COMPARTMENT 2023-37860<[01] REPLACED BRACKET AND FASTENERS LOC BS 400 AND LBL 21.80 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV:- SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REP
- [SDR SWAA2023021490067](https://openairdocs.org/sdr/SWAA2023021490067.md): Stringer · cracked · Jan 9, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-37865<[01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P301
- [SDR SWAA2023021490068](https://openairdocs.org/sdr/SWAA2023021490068.md): Gusset · cracked · Jan 9, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Plate/Skin
  > CRACK GUSSET LOC BS 500D AND STR 19L FWD CARGO COMPARTMENT 2023-37861<[01] REPLACED GUSSET LOC BS 500D AND STR 19L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9; 51-40-02 AND DRAWING 143A7902 REV:C; SEE INDIVIDUAL SIGNOFFS BELOW.;[02] INSTALLED NEW GU
- [SDR SWAA2023021489755](https://openairdocs.org/sdr/SWAA2023021489755.md): Support Angle · cracked · Jan 9, 2023 · N7825A · Boeing 7377CT · Wing Spar
  > CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR WEB BOOST PUMP IFSS 120 AT LT WING 2023-37834<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00HDJ3H;[02] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00HDJ3H
- [SDR SWAA2023021489745](https://openairdocs.org/sdr/SWAA2023021489745.md): Tie Clip · cracked · Jan 8, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Structure
  > CRACK TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN 2023-37813<[01] REPLACED TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 141A1110 REV:- SHEET:17 SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED.
- [SDR SWAA2023021489744](https://openairdocs.org/sdr/SWAA2023021489744.md): Stub Frame · cracked · Jan 8, 2023 · N7825A · Boeing 7377CT · Fuselage Main, Structure
  > CRACK FRAME STUB ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2023-37814<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] PERFORMED REPAIR ON FRAME STUB BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN IAW B737-700

Next page: https://openairdocs.org/aircraft/N7825A/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 = 'N7825A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7825A/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.