# Service difficulty reports: N952CA

A list on [N952CA](https://openairdocs.org/aircraft/N952CA.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 6 · 268 reports

- [SDR U2RA2026091100059](https://openairdocs.org/sdr/U2RA2026091100059.md): Bottle · low pressure · Sep 11, 2026 · N952CA · Boeing 747428 · Escape Slide
  > UPPER DECK DOOR SLIDE INFLATION CYLINDER PRESSURE LOW. REMOVED AND REPLACED DOOR SLIDE ASSEMBLY.
- [SDR U2RA2026081700049](https://openairdocs.org/sdr/U2RA2026081700049.md): Circuit Card · faulted · Aug 12, 2026 · N952CA · Boeing 747428 · Fire Detection
  > ON GROUND - ERRONEOUS FIRE WARNINGS - CLEANED AND RESEATED AFOLTS INTERFACE CARD. SYSTEM OPERATION NORMAL PER AIRCRAFT MAINTENANCE MANUAL 26-10-01.
- [SDR U2RA2026051200028](https://openairdocs.org/sdr/U2RA2026051200028.md): Longeron · cracked · Apr 19, 2026 · N952CA · Boeing 747428 · Fuselage Main, Structure
  > 2EA CRACK INDICATON FOUND AT BS2598 BULKHEAD R/H S-11R LONGERON P/N 65B02522-4 PER BOEING SR MUA-MUA-26-0026-22B REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12-2026 AND PER BCS 202603210023-0016
- [SDR U2RA2026051200027](https://openairdocs.org/sdr/U2RA2026051200027.md): Frame · cracked · Apr 1, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame
  > 1EA CRACK FOUND AT BS2598 BULKHEAD RHS OUTER CHORD HOLE C PER BOEING SR MUA-MUA-26-0022-07B REPAIR CARRIED OUT PER BOEING 8100-9 DATEED MAY, 12,2026.REFF BOEING BCS 202603210023-0016
- [SDR U2RA2026051200019](https://openairdocs.org/sdr/U2RA2026051200019.md): Stringer · cracked · Mar 26, 2026 · N952CA · Boeing 747428 · Fuselage Main, Longeron/Stringer
  > FCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA R/H 1160 AND STRINGER 10R REPAIR CARRIED OUT PER 8100-9 DATED 04/28/2026 REF BOEING COMMUNICATION SYSTEM MESSAGE NUMBERS FOR CASE # 06320986
- [SDR U2RA2026051200024](https://openairdocs.org/sdr/U2RA2026051200024.md): Frame · cracked · Mar 21, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame
  > ONE CRACK FOUND AT FRAME SUPPORT OF 747 SSID REV. H ITEMS F­49G ON THE RHS AREA OF THE HINGE FITTING. PER BOEING SR MUA­MUA­26­0026­03B. REPAIR CARRIED OUT PER BOEING 8100­9 DATED MAY 13 2026 AND REF BCS 202603130057­009
- [SDR U2RA2026051200025](https://openairdocs.org/sdr/U2RA2026051200025.md): Stringer · cracked · Mar 18, 2026 · N952CA · Boeing 747428 · Fuselage Main, Longeron/Stringer
  > FCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA L/H 1160 AND STRINGER 10L REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12, 2026 REF BCS 0632095
- [SDR U2RA2026051200018](https://openairdocs.org/sdr/U2RA2026051200018.md): Tension Tie · cracked · Mar 16, 2026 · N952CA · Boeing 747428 · Fuselage Main, Structure
  > OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS AT 1120 R/H TENSION TIE. REPAIR CARRIED OUT PER 8100=9 DATED 05/08/2026 REFF BOEING COMMUNICATION CASE 063200880
- [SDR U2RA202605000011](https://openairdocs.org/sdr/U2RA202605000011.md): Fastener · broken · Mar 10, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > LOCK FASTENER HEAD BROKEN AT TENSION TIE ATTACH FRAME LOCATED AT BS 1220 RT AND STRINGER 10R
- [SDR U2RA2026051200017](https://openairdocs.org/sdr/U2RA2026051200017.md): Doubler · cracked · Mar 9, 2026 · N952CA · Boeing 747428 · Empennage Structure
  > FINDING 002002 DOCUMENT FCD 744-53-0057-DURING C-CHECK 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR WAS COMPLTED PER FAA 8100-9 DATED 0/21/2006 ON BOEING SERVICE REQUEST 202603060065-0011.
- [SDR U2RA202604110007](https://openairdocs.org/sdr/U2RA202604110007.md): Doubler · cracked · Mar 9, 2026 · N952CA · Boeing 747428 · Horizontal Stabilizer, Plate/Skin
  > 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR COMPLETED PER:CASTLE ID: 202603060065: BOEING 8100-9 ISSUED DATED 04/21/2026. REF ID 202603060065-0011
- [SDR U2RA202604110006](https://openairdocs.org/sdr/U2RA202604110006.md): Web · cracked · Mar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON FORWARD FUSELAGE WEB OF THE NOSE GEAR WELL AT STRINGER 26, BS 160-180 CORRECTIVE ACTION: CAT B. REPAIR PER SRM. REINSPECT DUE AT 33,018 CYCLES
- [SDR U2RA2026033100003](https://openairdocs.org/sdr/U2RA2026033100003.md): Floor Support · cracked · Mar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > AFT CARGO INTERCOSTAL CRACK AT STA 1940 TO STA 1960, LBL77 PERFORMED REPAIR IAW SRM 51-70-13 R1
- [SDR U2RA202604280010](https://openairdocs.org/sdr/U2RA202604280010.md): Tension Tie · cracked · Mar 2, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > OPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING BS 1180LT - 1140 RT.
- [SDR U2RA2020405000005](https://openairdocs.org/sdr/U2RA2020405000005.md): Web · cracked · Mar 2, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON FORWARD FUSELAGE WEB OF NOSE GEAR WELL AT STRINGER S-26 STA 140-160 WL 205 R&R WEB PART NUMBER 65B01870U243 IAW SRM 51-40-02
- [SDR U2RA2026051100015](https://openairdocs.org/sdr/U2RA2026051100015.md): Tension Tie · cracked · Feb 26, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > OPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1180 L/H STA 1140 R/H. REPAIR COMPLETED PER BCS MESSAGE NUMBER 06316150 INSPECTION THRESHOLD 21,108 TOTAL FLIGHT CYCLES
- [SDR U2RA2026051100014](https://openairdocs.org/sdr/U2RA2026051100014.md): Frame · cracked · Feb 25, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame
  > WHILE IN C CHECK - PERFORMED SURFACE HFEC INSPECTION OF FCD 744-53-0017 R2 A 1 INCH CRACK WAS FOUND ON CHORD BETWEEN S-37R AND S-38R. REPAIR PERFORMED PER BOEING BCS MUA N952CA / 25238 FRAME CRACK BS 1140 RH, RBL 80 / WL 330.
- [SDR U2RA2025102600023](https://openairdocs.org/sdr/U2RA2025102600023.md): Bottle · low pressure · Oct 26, 2025 · N952CA · Boeing 747428F · Escape Slide
  > LH EMERGENCY SLIDE RESERVOIR PRESSURE IS BELOW GREEN BAND.
- [SDR U2RA2025021900012](https://openairdocs.org/sdr/U2RA2025021900012.md): Unknown · odor · Feb 13, 2025 · N952CA · Boeing 747428F · Air Distribution System
  > ON DESCENT ELECTRICAL BURNING SMELL. STATUS: EE CLNG EXH FAN. PERFORMED EE CLNG EXT FAN GROUND TEST PER AMM 21-58-00, TEST OF. INSPECTED ELECTRONIC EQUIPMENT COMPARTMENT FOR SUSPECTED BURNING AND CHECKED FOR ALL CBS, ALL OK. NO VISIBLE BURNS OR BURNING SMELL
- [SDR U2RA2025020300002](https://openairdocs.org/sdr/U2RA2025020300002.md): Fuel Panel · misinstalled · Feb 3, 2025 · N952CA · Boeing 747428F · Aircraft Fuel System
  > FUEL PANEL WAS INCORRECTLY SET AND CAUSED FUEL TO OVERBOARD THROUGH THE FUEL TANK VENT R/H. PANEL TESTED AND NO DEFECTS NOTED.
- [SDR U2RA2025011300070](https://openairdocs.org/sdr/U2RA2025011300070.md): Wire Harness · chafed · Jan 5, 2025 · N952CA · Boeing 747428F · Fuselage Main, Bulkhead Fuselage wiring
  > DURING A-CHECK AT LEVEL 5 KCNW, IT WAS DISCOVERED THAT A WIRE BUNDLE WAS CHAFFING WITH POST P/N: 65B14087-3 LOCATED AT FRAME STA. 460, LBL 87. THE DAMAGE WAS MEASURED AS 4MM X 5MM, WHICH IS OUT OF LIMITS. PERMANENT REPAIR ACCOMPLISHED IN ACCORDANCE WITH FVCI E
- [SDR U2RA2025011100069](https://openairdocs.org/sdr/U2RA2025011100069.md): Reservoir · low pressure · Jan 5, 2025 · N952CA · Boeing 747428F · Doors
  > DURING A-CHECK INSPECTION AT LEVEL 5 AEROSPACE KCNW, IT WAS FOUND THAT EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 HAS LOW PRESSURE. EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 WAS REMOVED AND REPLACED ON NR 0072 UNDER LEVEL 5 AEROS
- [SDR U2RA2024081500023](https://openairdocs.org/sdr/U2RA2024081500023.md): Pressure Deck · cracked · Aug 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Bulkhead
  > DURING C CHECK IN GMF, FOUND CRACK ON SKIN AT LH WLG W/W CANTED PRESSURE DECK STA 1241LBL 11.33 CATEGORY B REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH BOEING MESSAGE BOE MUA-MUA 24-0122
- [SDR U2RA202406040146](https://openairdocs.org/sdr/U2RA202406040146.md): Skin · cracked · Jun 4, 2024 · N952CA · Boeing 747428 · Fuselage Main, Structure
  > DURING C CHECK IN GMF FOUND CRACK ON SKIN AT LH WLG CANTED PRESSURE DECT STA 1241 LBL 11.33. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH BOEING MESSAGE NUMBER- BOE-MUA-24-0122
- [SDR U2RA2024081500040](https://openairdocs.org/sdr/U2RA2024081500040.md): Skin · damaged · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > FOUND RIVET HOLES ELOGATED ON SKIN 2700 LH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER BETWEEN.280 INCH UP TO.320 INCH
- [SDR U2RA2024081500039](https://openairdocs.org/sdr/U2RA2024081500039.md): Support Frame · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Aerodynamic Fairings
  > DURING MAINTENANCE C CHECK AT GMF FOUND LOWER FUSALAGE STA 1000 CENTER TO RH SIDE SUPPORT FRAME FOR BODY FAIRING CORRISON. REAPIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-70-12 (REV59/20FEB2024) AND WAS A CAT A REPAIR.
- [SDR U2RA2024081500038](https://openairdocs.org/sdr/U2RA2024081500038.md): Fairing · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFORMING C CHECK RH WING O/B AILERON UPPERSURFACE L/E FAIRING CRACK POS O/B SIDE REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV59 20FEB2024)
- [SDR U2RA2024082100022](https://openairdocs.org/sdr/U2RA2024082100022.md): Fairing · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFORMING C CHECK RH WING O/B AILERON UPPER SURFACE LE FAIRING CRACK POS CENTER REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59 20FEB2024.
- [SDR U2RA2024081500036](https://openairdocs.org/sdr/U2RA2024081500036.md): Bracket · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFORMING C CHECK RH WING O/B AILERON UPPER SURFACCE BRACKET FE FAIRING CRACK POS I/B SIDE. REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59 20FEB2024)
- [SDR U2RA2024081500035](https://openairdocs.org/sdr/U2RA2024081500035.md): Bracket · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFOMING C CHECK IN GMF RH WING O/B AILERON BRACKET BALLAST CORROSION POS #1 FROM O/B. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-56-02 REPAIR 1 (REV 59 20FEB2024)
- [SDR U2RA2024081500034](https://openairdocs.org/sdr/U2RA2024081500034.md): Structure · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Wing Main, Frame Structure
  > WHILE PERFOMING C CHECK IN GMF FOUND CORROSION ON LH WING L/E CHORD OLES 1530. THIS REPAIR IS CATEGORY A. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-41-13 REPAIR 1 & 51-70-11 (REV 59 20FEB 2024)
- [SDR U2RA2024081500033](https://openairdocs.org/sdr/U2RA2024081500033.md): Cargo Track · chafed · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE PERFORMING C CHECK IN GMF FOUND CHAFING ON FWD CARGO COMPARTMENT SEAT TRACK AT STA 570 RBL 45.5 THIS REPAIR IS CATEGORY A REPAIR WAS ACCOMPLICHED IN ACCORDANCE WITH SRM 53-00-52 REPAIR 10 (RREV 59 20FEB2024)
- [SDR U2RA2024081500032](https://openairdocs.org/sdr/U2RA2024081500032.md): Bracket · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFORMING C CHECK RH WING O/B AILRERON UPPER SURFACE BRAKET LE FAIRING CRACK POS I/B SIDE. REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59/20FEB2024)
- [SDR U2RA2024081500031](https://openairdocs.org/sdr/U2RA2024081500031.md): Support Frame · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Structure
  > WHILE PERFORMING C CHECK IN GMF FOUND CORRISION OUT OF LIMTS ON STA 1000 LBL 11.33-37.50 SUPPORT FRAME FOR BODY FAIRING THIS REPAIR IS CATIGORY A REPAIR WAS ACCOMPLISHE IN ACCORDANCE WITH THE SRM 51-70-12 (REV 59,20 FEB/2024
- [SDR U2RA2024081500030](https://openairdocs.org/sdr/U2RA2024081500030.md): Skin · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > RT SIDE FUSELAGE INNER WINDOW BELT CORROSION AT STA 1000 STR 15-STR 23
- [SDR U2RA2024081500029](https://openairdocs.org/sdr/U2RA2024081500029.md): Skin · damaged · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > FOUND RIVET HOLES ELOGATED ON SKIN RH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER IS BETWEEN.280 TO.320 INCH
- [SDR U2RA2024081500028](https://openairdocs.org/sdr/U2RA2024081500028.md): Skin · temp repair · Jun 1, 2024 · N952CA · Boeing 747428 · Standard Practices/Structures
  > DURING CHECK AT GMF FOUND TEMPERARY REPAIR AT LH WING LEADING EDGE WS 1000 THAT NEEDS REPLACED TO PERMANET REPAIR CATEGORY A REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-41-01 REPAIR 6 (REV 59/20 FEB 2023
- [SDR U2RA2024081500027](https://openairdocs.org/sdr/U2RA2024081500027.md): Skin · punctured · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons
  > WHILE PERFORMING C CHECK IN GMF RH WING AILERON LOWER SURFACE PUNCTURE REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59/20FEB 2024
- [SDR U2RA2024081500026](https://openairdocs.org/sdr/U2RA2024081500026.md): Web · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > DURING C CHECK IN GMF FOUND CRACK AT MED#1 RH UPPER SILL WEB CRACK AT STA 480 STR 16R CATEGORY B REPAIR WAS ACCOMPISHED IN ACCORDANCE WITH SRM 53-10-15 REPAIR 1 (REV 59/20 FEB 2024
- [SDR U2RA2024081500025](https://openairdocs.org/sdr/U2RA2024081500025.md): Reveal · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING C CHECK IN GMF FOUND CRACK AT MED#5 CUTOUT DOOR REVEAL AT STA 2240 STR 21 NEAR DOOR LOCK RELEASE THIS REPAIR IS ACCOMPLISHED ANS CATOGORIZED AS CAT A REPAIR IN ACCORDANCE WITH SRM 53-60-15 REPAIR 7 (REV 59/20 FEB 2024
- [SDR U2RA2024081500024](https://openairdocs.org/sdr/U2RA2024081500024.md): Pressure Deck · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Bulkhead
  > WHILE PERFOMING C CHEHCK IN GMF, FOUNF CRACK ON SKIN AT RH W/G W/W CANTED PRESSURE DECK SURFACE SKIN AT STA 1241 RBL 5.5 CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-51 REPAIR 6 (REV 59, 20 FEB /2024
- [SDR U2RA2024031500004](https://openairdocs.org/sdr/U2RA2024031500004.md): Battery · no test · Feb 19, 2024 · N952CA · Boeing 747428 · Emergency Exits
  > UPPER DECK RIGHT EMERGENCY DOOR BATTER TEST FAIL - REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MAINTENANCE MANUAL. OPS CHECK OK.
- [SDR U2RA2024012300001](https://openairdocs.org/sdr/U2RA2024012300001.md): Nose Cowl · dented · Jan 22, 2024 · N952CA · Boeing 747428 · Engine Cowling System
  > AIRCRAFT SUSTAINED DAMAGE TO #4 ENGINE NOSE COWL DURING GROUND HANDLING. ACCOMPLISHED TEMPORARY REPAIR TO NOSE COWL PER FVCI EO 24009-1. THIS IS A TEMPORARY REPAIR AND WILL REQUIRED PERMANENT REPAIR OR COWL REPLACEMENT.
- [SDR U2RA2023091100044](https://openairdocs.org/sdr/U2RA2023091100044.md): Skin Panel · gouged · Sep 11, 2023 · N952CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > DURING OFF-LOADING OF CARGO, CARGO LOADING VEHICLE STRUCK THE SEAL DEPRESSOR AT THE FORWARD LOWER CORNER OF THE DOOR CUT-OUT. DAMAGE OCCURRED TO AN EXISTING REPAIR DOUBLER; REFER TO AML #63577-2 AND FVCI E.O. 23184-1 REV. IR DATED 09/08/2023. DAMAGED DOUBLER
- [SDR U2RA2023081500040](https://openairdocs.org/sdr/U2RA2023081500040.md): Lamp · inoperative · Aug 14, 2023 · N952CA · Boeing 747428 · Emergency Lighting
  > DURING A-CHECK WO 230107, MRO HANGAR 901 DISCOVERED A MID EMERGENCY LIGHT IN FLIGHT DECK WAS NOT ILLUMINATING. THE LIGHT BULB WAS REPLACED WITH AN ILLUMINATION TEST PRODUCING SATISFACTORY RESULT. SEE HANGAR 901 (CRS: HAIY901D) PROJECT# H1-23-05-00084, WO 18590
- [SDR U2RA2023081100039](https://openairdocs.org/sdr/U2RA2023081100039.md): Cartridge · out of tolerance · Aug 8, 2023 · N952CA · Boeing 747428 · Emergency Exits
  > DURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, LEFT HAND UPPER DOOR, DISCHARGE CARTRIAGE FOR THE PRESSURE VESSEL M7039 FAILED THE RESISTANCE CHECK. WORK ACCOMPLISHED ON CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 1859
- [SDR U2RA2023081100038](https://openairdocs.org/sdr/U2RA2023081100038.md): Cartridge · no test · Aug 8, 2023 · N952CA · Boeing 747428 · Emergency Exits
  > DURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, RIGHT HAND UPPER DOOR, BATTERY PACK M7038 FAILED TO TEST ON PRESS-TO-TEST SWITCH. WORK ACCOMPLISHED ON (CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 18590, NR 0047.
- [SDR U2RA2023081100037](https://openairdocs.org/sdr/U2RA2023081100037.md): Cartridge · no test · Aug 8, 2023 · N952CA · Boeing 747428 · Emergency Exits
  > DURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, LEFT HAND UPPER DOOR, BATTERY PACK M7037 FAILED TO TEST ON PRESS-TO-TEST SWITCH. WORK ACCOMPLISHED ON (CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 18590, NR 0046.
- [SDR 2023F00140](https://openairdocs.org/sdr/2023F00140.md): Unknown · unknown · May 15, 2023 · N952CA · Boeing 747428 · Flight Control System
  > DURING INSPECTION FOR ROUTINE WO 18360 – 0137 (SB TABLE 2 - INBOARD FLAP INSPECTION/LUBRICATION - AD 2021-02-15 (G)). IT WAS FOUND THAT ON SEQUENCE CARRIAGE NR 5 (R/H WING INBOARD FOREFLAP TRACK# 5), THE NUT ITEM NO. 11, WASHER ITEM NO. 12, OUTER CLAMP-UP WAS
- [SDR U2RA2023040300018](https://openairdocs.org/sdr/U2RA2023040300018.md): Unknown · unknown · Mar 31, 2023 · N952CA · Boeing 747412 · Wing, Control Surfaces
  > DURING ROUTINE INSPECTION, FOUND RIGHT INBOARD MID FLAP WITH GROUND DAMAGE (DENTED). ACCOMPLISHED A TIME LIMITED MAJOR REPAIR PER FLIGHT VEHICLES CONSULTING ENGINEERING ORDER 23069-1. DATA APPROVED ON FAA FORM 8110-3 DATED 3/31/2023 BY R. MANASHI DERT-876272

Next page: https://openairdocs.org/aircraft/N952CA/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 = 'N952CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N952CA/reports

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