# Service difficulty reports: N919CA

A list on [N919CA](https://openairdocs.org/aircraft/N919CA.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 · 195 reports

- [SDR U2RA2026102400066](https://openairdocs.org/sdr/U2RA2026102400066.md): Power Supply · faulted · Oct 20, 2026 · N919CA · Boeing 747428 · Emergency Lighting
  > UPPER DECK EMER LIGHT POWER SUPPLY M5056 NOT OPERATE. REPLACED UPPER DECK EMER LIGHT POWER SUPPLY (M5056) AND EMER LIGHT CHECK NORMAL AND THEN POWER SUPPLY TEST SWITCH CHECK NORMAL PER AMM 33-51-04-11 ITEM 345.
- [SDR U2RA2026072100045](https://openairdocs.org/sdr/U2RA2026072100045.md): Frame · cracked · Jun 29, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION FOUND 2 CRACK HOLES AT R5 DOOR INNER CHORD STA 2231 S-19. PERFORMED CLASS B REPAIR IAW SRM 53-60-15, REPAIR 2.
- [SDR U2RA2026070800032](https://openairdocs.org/sdr/U2RA2026070800032.md): Skin · dented · Jun 25, 2026 · N919CA · Boeing 747428 · Trailing Edge Flaps
  > DURING AIRCRAFT C-CHECK IN ICN (INCHEON, SOUTH KOREA) SHARP TECHNICS K MAINTENANCE DISCOVERED CHAFE DAMAGE ON THE UPPER SURFACE OF THE INBOARD TRAILING EDGE AFT FLAP OUTER SKIN PANEL P/N 65B02077-508. PERFORMED PERMANENT REPAIR IAW FLIGHT VEHICLES CONSULTING,
- [SDR U2RA2026072100046](https://openairdocs.org/sdr/U2RA2026072100046.md): Frame · cracked · Jun 24, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > CRACK FOUND AT RH STA 1140 LH TENSION TIE FRAME. REPAIRS COMPLETED PER BCS CASE 06373559.
- [SDR U2R2026F00000](https://openairdocs.org/sdr/U2R2026F00000.md): Frame · cracked · Jun 19, 2026 · N919CA · Boeing 747428 · Fuselage Miscellaneous Structure
  > DURING OPEN HOLE INSPECTION, DETECTED DEFECT SIGNAL AT FRAME WEB BS 1265. PERFORMED REPAIR IAW NAL FCD 744-53-0014 AND DWG 624U0060.
- [SDR U2RA2026071100033](https://openairdocs.org/sdr/U2RA2026071100033.md): Skin · damaged · Jun 19, 2026 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > .LIGHTNING-STRIKE DAMAGE FOUND ON THE FUSELAGE SKIN AT STA 225, STRINGER S-23R. PERFORMED REPAIR IAW BOEING BCS CASE MUA-MUA-26-0085. DATA APPROVED BY FAA FORM 8100-9 DATED 06/28/2026.
- [SDR U2RA2026072100044](https://openairdocs.org/sdr/U2RA2026072100044.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > CRACK FOUND IN OPEN HOLE INSPECTION AT RT STA 1120 TENSION TIE FRAME WEB 65B01749-22. REPAIRS COMPLETED PER BOEING BCS CASE 06372730
- [SDR U2RA2026072000041](https://openairdocs.org/sdr/U2RA2026072000041.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > A CRACK DAMAGED WAS FOUND ON THE FRAME WEB AT STA 1160 AND BETWEEN S-9R- 10R WHILE PERFORMING SERVICE BULLETIN 747-53A2702 REV 02. PERFORMED CLASS B REPAIR PER CASE 06372691
- [SDR U2RA2026072000040](https://openairdocs.org/sdr/U2RA2026072000040.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > DURING OPEN HOLE INSPECTION, CRACK FOUND AT BS 800 BETWEEN S-16R & S-17R. PERFORMED PERMANENT REPAIR AIW BOEING BCS MUA-MUA-26-0081-09B AND DWG 65B26468.
- [SDR U2RA2026072000039](https://openairdocs.org/sdr/U2RA2026072000039.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > DURING OPEN HOLE INSPECTION, 2 CRACKS FOUND AT BS800 BETWEEN S-15L TO S-17L. PERFORMED CLASS B REPAIR IAW BCS CASE # 06372411
- [SDR U2RA2026072100047](https://openairdocs.org/sdr/U2RA2026072100047.md): Tension Tie · cracked · Jun 14, 2026 · N919CA · Boeing 747428 · Fuselage Main, Attach Fittings
  > CRACK FOUND DURING OPEN HOLE INSPECTION AT L/H STA1180 TENSION TIE FWD CHANNEL. PERFORMED CLASS B REPAIR IAW SRM 53-40-30-2R-2.
- [SDR U2RA2026071900038](https://openairdocs.org/sdr/U2RA2026071900038.md): Tension Tie · cracked · Jun 11, 2026 · N919CA · Boeing 747428 · Fuselage Main, Attach Fittings
  > OPEN HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1140 R/H TENSION TIE. REPAIR COMPLETED PER BCS MESSAGE 06370241 INSPECTION THRESHOLD 20,811 TOTAL FLIGHT CYCLES.
- [SDR U2RA2026051200026](https://openairdocs.org/sdr/U2RA2026051200026.md): Frame · cracked · Apr 10, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > 1EA CRACK FOUND AT BS2598 BULK HEAD RHS FRAME SUPPORT HOLE D AS PER BOEING SR MUA-MUA-26-0022-07B REPAIRED CARRIED OUT PER BOEING 8100-9 DATED MAY 12 2026 AND PER BOEING BCS 202603210023-0016
- [SDR U2RA2026032500002](https://openairdocs.org/sdr/U2RA2026032500002.md): Lamp · inoperative · Mar 18, 2026 · N919CA · Boeing 747428 · Emergency Lighting
  > U/D EMEGENCY LIGHT NO ON QTY 3 EA. REPLACED THE LAMP AND OPERATION CHECK PER AMM 33-51-07 FOUND NORMAL
- [SDR U2RA2025082100020](https://openairdocs.org/sdr/U2RA2025082100020.md): Skin · cracked · Aug 22, 2025 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > DURING A CHECK AT RKSI, WHILE PERFORMING FCD 744-53-0076 R2, 250 FLIGHT CYCLE (FC) REPETITIVE INSPECTIONS FOR SCRIBE LINE FINDINGS ON SB 747-53A2563 LIMITED RETURN TO SERVICE (LRTS) PROGRAM, IT WAS DISCOVERED THAT SKIN PANEL 33L WITH P/N: 65B04135-343 HAVE 02
- [SDR U2RA2024090600054](https://openairdocs.org/sdr/U2RA2024090600054.md): Engine · faulted · Aug 30, 2024 · N919CA · Boeing 747428 · Engine (Turbine/Turboprop)
  > DURING TAKE-OFF ROLL, SHORTLY AFTER SELECTING "TOGA", ENGINE NUMBER 4 SHOWED RED EGT INDICATION AS AIRCRAFT VEERED SIGNIFICANTLY TO THE LEFT. LOW SPEED (APPROXIMATELY 40 KTS.) RTO CARRIED OUT. ENGINE NUMBER 4 WAS DETERMINED UNSERVICEABLE AND REPLACED PRIOR T
- [SDR U2RA2024081500022](https://openairdocs.org/sdr/U2RA2024081500022.md): Power Supply · no test · Aug 15, 2024 · N919CA · Boeing 747428 · Emergency Lighting
  > WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTS, POWER PACK AND ATTENDANT SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION M5056 STA LBL 6
- [SDR U2RA2024081500021](https://openairdocs.org/sdr/U2RA2024081500021.md): Power Supply · failed · Aug 15, 2024 · N919CA · Boeing 747428 · Emergency Lighting
  > WHILE PERFORMINNG OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PIPLOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER TO POSITON M5055 STA 610 LBL 88.
- [SDR U2RA2024081520](https://openairdocs.org/sdr/U2RA2024081520.md): Power Supply · no test · Aug 15, 2024 · N919CA · Boeing 747428 · Exterior Lighting
  > WHILE PERFORMING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL. EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION - M5057 STA 717 LBL 8
- [SDR U2RA2024081519](https://openairdocs.org/sdr/U2RA2024081519.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CRACK ON SEAT TRACK BETWEEN STA 980 AND STA 1000 LBL 75 (MAIN DECK)
- [SDR U2RA2004081518](https://openairdocs.org/sdr/U2RA2004081518.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 980 AND STA 1000 RBL 75 FOUND CRACK ON SEAT TRACK.
- [SDR U2RA2004081517](https://openairdocs.org/sdr/U2RA2004081517.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CRACKON SEAT TRACK FWD CARGO STA 580, RBL 24
- [SDR U2RA2024070300013](https://openairdocs.org/sdr/U2RA2024070300013.md): Battery Pack · discharged · May 20, 2024 · N919CA · Boeing 747428 · Emergency Lighting
  > DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5056 AT BS 663, LBL 8, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.
- [SDR U2RA2024070300012](https://openairdocs.org/sdr/U2RA2024070300012.md): Battery Pack · discharged · May 20, 2024 · N919CA · Boeing 747428 · Emergency Lighting
  > DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5057 AT BS 717, LBL 8, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.
- [SDR U2RA2024070300011](https://openairdocs.org/sdr/U2RA2024070300011.md): Battery Pack · discharged · May 20, 2024 · N919CA · Boeing 747428 · Emergency Lighting
  > DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5055 AT BS 610, LBL 88, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.
- [SDR U2RA2024022000003](https://openairdocs.org/sdr/U2RA2024022000003.md): Relay · broken · Feb 19, 2024 · N919CA · Boeing 747428 · Fire Protection System Wiring
  > ENGINE INDICATING CREW ALERTING SYSTEM (EICAS) MESSAGE "FIRE MN DK MID". - BENT PIN DISCOVERED ON LOOP B RELAY R5168 CAUSING INTERMITTANT LOOP B FIRE WARNING INDICATION. REPLACED RELAY R5168. LOOP B FUNCTIONS NORMAL PER AIRCRAFT MAINTENANCE MANUAL 26-10-00
- [SDR U2RA2023073000037](https://openairdocs.org/sdr/U2RA2023073000037.md): Bulb · inoperative · Jul 27, 2023 · N919CA · Boeing 747428 · Emergency Lighting
  > DURING SCHEDULED A-CHECK MAINTENANCE, AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHT SYSTEM RESULTED IN FINDING OF INOPERATIVE LIGHT BULB AT THE UPPER DECK STAIRS POSITION. REMOVED AND REPLACED LAMP. OPS GOOD IAW AMM 33-51-00. OPS GOOD.
- [SDR U2RA2023041000019](https://openairdocs.org/sdr/U2RA2023041000019.md): Cowling · damaged · Apr 8, 2023 · N919CA · Boeing 747428 · Engine Thrust Reverser
  > #4 ENGINE INBOARD THRUST REVERSER TRANSLATING COWL DAMAGED BEYOND LIMITS. REPAIRED PER FVCI ENGINEERING ORDER #23075-1.
- [SDR U2RA2022072800037](https://openairdocs.org/sdr/U2RA2022072800037.md): Tension Tie · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, L/H BS1140 FRAME WEB & FRAME FOUND CRACK. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-07 REPAIR 2, REV 115. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN4056.
- [SDR U2RA2022072800036](https://openairdocs.org/sdr/U2RA2022072800036.md): Tension Tie · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE INSPECTION, TENSION TIE - L/H BS 1180 FWD CHANNEL (REPAIRED PART) FOUND CRACK. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-30-2R-2 REPAIR 2, REV 54. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN3561.
- [SDR U2RA2022072800035](https://openairdocs.org/sdr/U2RA2022072800035.md): Frame · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Main, Frame
  > DURING INCORPORATION OF NAL FCD NO. 744-53-0061 R1 (SB 747-53A2450 REV 8) TO DO INSPECTION OF #5 MED LEFT, SECTION 46 BS 2231 FRAME, STR 15L THROUGH 15R, 1 EA HOLE WAS FOUND CRACKED ON LH FRAME INNER CHORD (P/N: 65B01849-51) FWD FLANGE AND STRAP (P/N: 65B01
- [SDR U2RA2022072800034](https://openairdocs.org/sdr/U2RA2022072800034.md): Pylon · damaged · Jul 15, 2022 · N919CA · Boeing 747428 · Nacelle/Pylon, Plate/Skin
  > IT WAS DISCOVERED AN ELONGATED FASTENER HOLE IN THE NO.2 PYLON INBOARD SKIRT PANEL FAIRING, P/N 311U2170-99, AT NAG STA 354. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-10, REV A, WHICH WA
- [SDR U2RA2022072800033](https://openairdocs.org/sdr/U2RA2022072800033.md): Seat Track · damaged · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Internal Mounting Structure
  > SEAT TRACK (P/N: 65B38272-1) ON CABIN MAIN DECK STA 1481 -1766, LBL 11.33 WAS FOUND BROKEN, THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-9, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3
- [SDR U2RA2022072800032](https://openairdocs.org/sdr/U2RA2022072800032.md): Shear Web · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Ventral Structure
  > IT WAS FOUND 2 EA CRACKS ON THE VERTICAL STABILIZER T/E BEAM RHS WEB (P/N: 173U1010-31) APPROX.AT RUD STA 307 AND RUD STA 332. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-8, REV IR, WHI
- [SDR U2RA2022072800031](https://openairdocs.org/sdr/U2RA2022072800031.md): Cowling · worn · Jul 15, 2022 · N919CA · Boeing 747428 · Engine Cowling System
  > WEAR DAMAGE WAS FOUND ON NO.3 ENG RH CORE COWL (P/N:224M4761-539, S/N: 1099) FWD FRAME EXISTING REPAIR. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-7, REV LR, WHICH WAS APPROVED BY FA
- [SDR U2RA2022072800030](https://openairdocs.org/sdr/U2RA2022072800030.md): Bulkhead Web · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Main, Bulkhead
  > BULKHEAD WEB (P/N: 6B815085-1077) WAS FOUND CRACKED AT STA 1480 BETWEEN WL140 AND WL 152. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-6, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATE
- [SDR U2RA2022072800029](https://openairdocs.org/sdr/U2RA2022072800029.md): Access Panel · elongated · Jul 15, 2022 · N919CA · Boeing 747428 · Nacelle/Pylon, Plate/Skin
  > DURING SCHEDULED INSPECTION, 2EA FASTENER HOLES ON 462ER DOOR ASSY (P/N: 311 U2060-110) C/T NO.2 PYLON RHS WERE FOUND ELONGATED. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22089-5, REV A, WHICH
- [SDR U2RA2022072800028](https://openairdocs.org/sdr/U2RA2022072800028.md): Seat Track · damaged · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Internal Mounting Structure
  > SEAT TRACK ON M/D STA 1265-1480, RBL 11.33 WAS FOUND BROKEN AND NO APPLICABLE REPAIR IN 747-400SF SRM. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22089-4, REV LR, WHICH WAS APPROVED BY FAA FORM
- [SDR U2RA2022072800027](https://openairdocs.org/sdr/U2RA2022072800027.md): Cowling · dented · Jul 15, 2022 · N919CA · Boeing 747428 · Engine Cowling System
  > IT WAS DISCOVERED (3 EA.) ELONGATED FASTENER HOLES IN THE OUTER SKIN OF THE RIGHT CORE COWL (P/N 224-2302-545, S/N 0619) CURRENTLY INSTALLED ON AIRCRAFT N919CA LOCATED AT APPROXIMATE NAS STA. 307.00, THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLI
- [SDR U2RA2022072800026](https://openairdocs.org/sdr/U2RA2022072800026.md): Skin Panel · dented · Jul 15, 2022 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > DURING ROUTINE MAINTENANCE IN HHN (KIRCHBERG, GERMANY), MAINTENANCE DISCOVERED TWO DENTS WITH GOUGES AT STA 5QO-520, S-22L-23L. CATEGORY 8 REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22032-2, REV D, WHICH
- [SDR U2RA2022072800025](https://openairdocs.org/sdr/U2RA2022072800025.md): Panel · cracked · Jul 15, 2022 · N919CA · Boeing 747428 · Nacelle/Pylon, Plate/Skin
  > IT WAS DISCOVERED CRACKS IN THE NO. 1 PYLON SKIRT BEAM OUTBOARD PANEL ASSEMBLY NEAR NAC STA 329. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-1, REV 8, WHICH WAS APPROVED BY FAA FORM 8110-
- [SDR U2RA2021060200018](https://openairdocs.org/sdr/U2RA2021060200018.md): Power Supply · inoperative · Jun 2, 2021 · N919CA · Boeing 747428 · Emergency Equipment
  > UPPER DECK RIGHT DOOR EMERGENCY BOTTLE SQUIB BATTERY TEST INOPERATIVE. - REMOVED AND REPLACED UPPER DECK DOOR BOTTLE SQUIB BATTERY IAW B747-400 AIRCRAFT MAINTENANCE MANUAL 52-23-14.
- [SDR U2RA2021042300014](https://openairdocs.org/sdr/U2RA2021042300014.md): Support · cracked · Apr 20, 2021 · N919CA · Boeing 747428 · Aerodynamic Fairings
  > REFER TO LP 43984-3 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1620, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 162
- [SDR U2RA2021042300013](https://openairdocs.org/sdr/U2RA2021042300013.md): Support · cracked · Apr 20, 2021 · N919CA · Boeing 747428 · Aerodynamic Fairings
  > REFER TO LP 43984-1 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1540, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 154
- [SDR U2RA2021040200010](https://openairdocs.org/sdr/U2RA2021040200010.md): Hydraulic Line · cracked · Apr 1, 2021 · N919CA · Boeing 747428 · Hydraulic System, Main
  > REFERENCE NATIONAL AIRLINES AML 44070-1: DURING TAXI, SMELLED BAD HYDRAULIC ODOR AND RETURNED TO GATE. FOUND HYDRAULIC LEAK IN SYSTEM #1 HYDRAULIC LINE, LEFT SIDE FUSELAGE AT BS 900. REPLACED SUBJECT HYDRAULIC LINE WITH TEMP "FLEXIBLE" HYDRAULIC LINE IAW B7
- [SDR U2RA2021030400002](https://openairdocs.org/sdr/U2RA2021030400002.md): Fmc · failed · Jan 23, 2021 · N919CA · Boeing 747428 · Flight Management Computing Hardware System
  > DISCREPANCY: LP 43593 - AIRCRAFT ENCOUNTERED A FAULT IN THE RIGHT FLIGHT MANAGEMENT COMPUTER (FMC). SIMULTANEOUSLY WITH THIS FAULT, AN AUTO-PILOT (A/P) CAUTION ILLUMINATED WITH AN UNCOMMANDED "NOSE DOWN" PITCH IN THE AIRCRAFT WITH THE A/P ENGAGED. IMMEDIATE
- [SDR U2RA2020082000001](https://openairdocs.org/sdr/U2RA2020082000001.md): Access Panel · missing · Aug 5, 2020 · N919CA · Boeing 747428 · Nacelle/Pylon, Plate/Skin
  > UPON WALK-AROUND, FOUND NR 1 PYLON ACCESS PANEL 452FR MISSING. INTERIM ACTION: INSTALLED INTERIM REPAIR, AS PER GMM 13.1.3. ITEM APPROVED FOR ACI, AS PER GMM 3.8.11 AND GMM 13.1.3. ITEM TRANSFERRED TO DMI 200006-600 CAT "ACI", DUE AT NEXT STATION WITH ADEQ
- [SDR U2RA2020042540001](https://openairdocs.org/sdr/U2RA2020042540001.md): Relay · inoperative · Apr 24, 2020 · N919CA · Boeing 747428 · Trailing Edge Flap Control System
  > FLAPS CONTROL EICAS MESSAGE DISPLAYED ON FINAL APPROACH. PERFORMED GO AROUND, COMPLETED CHECKLIST AND LANDED WITHOUT INCIDENT. - CENTRAL MAINTENANCE COMPUTER MESSAGES 27600, 27601, AND 27602 FOUND ACTIVE, FLAP CONTROL UNIT LEFT, RIGHT, AND CENTER FAIL. REMOV
- [SDR U2RA2020042040001](https://openairdocs.org/sdr/U2RA2020042040001.md): Skin · damaged · Apr 14, 2020 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED SECTION 48, BODY STATION 2655 TO 2689, STRINGER 5L TO 11L - ACCOMPLISHED MAJOR REPAIR OF DAMAGE IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. ENGINEERING ORDER CONTROL NUMBER 20138 REVISION A DATED APRIL 15, 2020, DATA APPROVED ON
- [SDR U2RA201910220001](https://openairdocs.org/sdr/U2RA201910220001.md): Valve · stuck · Oct 22, 2019 · N919CA · Boeing 747428 · Fuel Storage
  > DURING REFUELING, THE RIGHT HAND SURGE TANK STARTED VENTING FUEL. - FOUND NUMBER 4 MAIN TANK REFUEL VALVE STICKING IN THE PARTIALLY OPEN POSITION. EXERCISED THE VALVE MANUALLY AND SYSTEM OPERATIONAL CHECK WAS NORMAL IN ACCORDANCE WITH B747-400 AIRCRAFT MAINTE

Next page: https://openairdocs.org/aircraft/N919CA/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 = 'N919CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N919CA/reports

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