N71411
Service difficulty reports · 69
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N71411' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N71411' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2026101920461Hmu · faultyREJECTED TAKEOFF AT APPROX 90 KIAS DUE TO E2 NOT ACHIEVING REQD T/O THRUST. REMOVED HMU, REMOVED FUEL PUMP PACKAGE IAW AMM 73-11-01-000-801-F00. INSTALLED NEW HMU & FUEL PUMP.SDR CALA2026101920450Shaft · shearedENGINE 2 NEVER ACHIEVED REQUIRED T/O THRUST. 90.6 REQUIRED. 90.0 ACHIEVED. FOUND ENG 2 FUEL PUMP DRIVE SHAFT SHEARED. REPLACEMENT OF FUEL PUMP PERFORMED. ENG 2 ACHIEVED 99.9% N1 AFTER PUMP WAS REPLACED. OPS CHECK NORMAL.SDR CALA2026041315318Pitot Head · cloggedIAS DISAGREE ON PFD DURING TAKEOFF AROUND 120 KIAS. PROBLEM WAS INTERRMITENT IN FLIGHT. DURING T/S FOUND HEAD OF MUD DAUBER WASP AND REMOVED FROM CAPT'S PITOT PROBE. SEE PIC. BLEW OUT CAPT'S AND F/O'S PITOT LINES FROM ADM'S NO OTHER RESTRICTIONS FOUND. RECSDR CALA2026021813886Lens · detachedEMERGENCY LIGHT AT ROW 22DEF HANGS DOWN REQUESTING MEL 3315A. COVER IS SECURED. REPLACED 22DEF AREA EMERGENCY LIGHT LENS IAW AMM 33-51-03. OPS CHECKED NORMAL, PLACARD REMOVED.SDR CALA2025120811875Battery Pack · inoperativeEMERGENCY LIGHT ABOVE SEAT ROW 12DEF INOPERATIVE. REMOVED UNSERVICEABLE BATTERY PACK AT BATTERY SUPPLY UNIT M1695 IAW AMM 33-51-06. INSTALLED SERVICEABLE BATTERY PACK IAW AMM 33-51-06. PERFORMED OPS TEST OF NEW SERVICEABLE BATTERY PACK IAW AMM 33-51-06, SUSDR CALA2025120511801Battery Pack · inoperativeFIRST CLASS EEPL LIGHTING AND R1 DOOR EMERGENCY LIGHTING INOP. SUPPORT TASK NSA EMX N/R 00159. REMOVED FWD ENTRY PANEL IAW AMM 25-21-71-000-807 SUBTASK 25-21-71-010-010. REMOVED BATTERY PACK AT BATTERY SUPPLY UNIT M1674 IAW AMM 33-51-06. INSTALLED SERVICEABLSDR CALA2025120411765Attach Angle · crackedSTATION 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY LBL 9.0. REPAIRED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.SDR CALA2025120411756Attach Angle · crackedBS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROX RBL 9.0. REPAIRED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.SDR CALA2025120411754Fitting · crackedSHEAR FITTING AT BS 540, RBL 15.04 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000 REV ORIGINAL.SDR CALA2025120411752Fitting · crackedSHEAR FITTING AT BS 540, LBL 15.04 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.SDR CALA2025120411749Fitting · crackedSHEAR FITTING AT BS 540, LBL 40.87 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.SDR CALA2025120411747Fitting · corrodedSHEAR FITTING AT BS 540, LBL 32.40 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.SDR CALA2025120411745Fitting · crackedSHEAR FITTING AT BS 540, LBL 6.14 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND DWG 111A2000, REV ORIGINALSDR CALA2025112711508Stringer · crackedINSIDE FUEL PANEL 532RB STRINGER U9 HAS A CRACK IN END OF STRINGER AND APPEARS TO END IN FASTENER HOLE. REPAIRED L/W U9 STRINGER END IAW UAL ECRA 5720-03581 REV ORIGINAL USING FASTENER OPTION C AND UAL AVO INT-11172025-0411-1 WITH NO DEVIATIONSSDR CALA2025100609611Bumper · faultedOVERWING EXIT SEAT ROW 15ABC, RED EMERGENCY ESCAPE LIGHT BROKEN THROUGH AND INSIDE THE BUMPER ASSY. R & R SEAT 15C BUMPER ASSY PER PINNACLE CMM. EMERGENCY LIGHT OPS CHK OK. PARTS USED: 29-2500-3-0199, QTY :1SDR CALA2025093009445Anti-Ice Valve · faultedCOWL ANTI-ICE NR 2 ENG ILLUMINATED AT FL390. QRH FOLLOWED. LIGHT STILL ON. ON ARRIVAL OVERHEAD FAULT LIGHT FOR E2 ANTI-ICE VALVE EXTINGUISHED. IAW AMM 30-21-11/401 REPLACED COWL ANTI ICE VALVE AS PRECAUTION. ENGINE IDLE LEAK CHECK GOOD. BONDING TEST GOOD ATSDR CALA2025050804562Idg · faultedRT SOURCE OFF LIGHT AND DRIVE LIGHT ILLUMINATED ON GEN2 DRIVE DISCONNECT GEN2 HAD ZERO VOLTS PART VERIFICATION FOR GENERATOR ASSY- INTEGRATED DRIVE PART # 761574B M&E 29-2411-9-0001 S/N AAAH010035 REF AIPC 24-11-11-01A FIG ITEM 5. REMOVED AND REPLACED NUMBERSDR CALA2025042904304Slide · not reportedR2 DOOR SLIDE REQUIRES REPLACEMENT. REMOVED AND REPLACED R2 DOOR MOUNTED SLIDE REF AMM 25-66-01-400-801. (LOG PAGE FOR PARTS TRACKING ONLY). ROTABLE PARTS CHG:TT # 1450279 SN OFF 0469 PN OFF 29-2566-9-0007.SLIDE, FWD/AFT OFF 29-2566-9-0007 0469 ON 29-2566-9-SDR CALA2024122601658Target · faultyLEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 1 LOCKED BY TOMC DURING VISUAL INSPECTION FOUND SL1 OUTBD PROX SENSOR TARGET BROKEN. REMOVED AND REPLACED SL1 OUTBD PROX SENSOR TARGET BRACKET REF SRM 51-40-02 ADJUSTED SLAT 1 PROX SENSOR S994 PER AMM TASK 27-88-11-40SDR CALA2024090600581Transmitter · faultyFLAPS- TRAILING EDGE FLAPS ASYMMETRY ON LANDING SEE ATTACHED PHOTO ADDING PICTURE OF DFD REPORT. DFD SHOWING LEFT T/E FLAP POSITION XMITTER LAGGING. REMOVED AND REPLACED LH FLAP POSITION TRANSMITTER PER AMM FLAP POSITION TRANSMITTER - REMOVAL/INSTALLATION REFESDR CALA2024050801409None · noneBIRDSTRIKE NOSE AREA, CLEANED UP BIRD STRIKE AREA AND PERFORMED INSPECTION PER AMM 05-51-18-210-802-C1 AND 05-51-18-210-801. NO DAMAGE FOUND. NO FURTHER DEFECTS NOTED. AC OKAY FOR SERVICE. INSPECTED F/O WINDSHIELD WIPER FOR DAMAGE REF AMM TASK 30-42-31-820-801SDR CALA2023062802045Fastener · missingPDA 1 PASSENGER REPORTS MISSING FASTENERS RIGHT WING LEADING EDGE INBOARD OF THE NO.2 ENGINE. INSPECTED RIGHT WING INBOARD FIXED LEADING EDGE UPPER SKIN. FOUND LOOSE AND DAMAGED FASTENERS AND NO MISSING FASTENERS. REMOVED AND REPLACED LOOSE AND DAMAGED FASTENESDR CALA2023040601053Fuse · faultyEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - RED EMERGENCY LIGHTS INOP AT SEAT ROWS 15ABC, 20ABC, & 21ABC. R & R FAULTY FUSE AT POWER SUPPLY M1694 JUST FWD OF LH FWD OVERWING EMERGENCY DOOR. ALL EMERGENCY LIGHTS OPS CHK OK. PARTS USED: 00-0SDR CALA2022121903421Stop Fitting · damagedPDA 3 LEFT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED & MISSING A SECTION ENTIRE LENGTH -- SEE PHOTO PHOTO ADDED PARTS ADDED REF IPC 21-51-03-06A AND IPC 21-51-03-05ASDR CALA2022102402939None · noneLE FLAP TRANSIT LT ON REPLACED #1SLAT INBOARD SENSOR. OPS CHECK GOOD.SDR CALA2022090702290None · crackedLH HORZ STAB STA 92.70 VERTICAL RIB STIFFENER #3 CRACKED. LH HOR Z STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STI FFENER #3 CRACK REPAIR.CUTOUT SKIN STA 92.70 AT VERTICAL STIFFEN ER #3 IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11 STEP 4.(2). VERI SDR CALA2022090702289None · noneL/H HORIZONTAL STAB LOWER SKIN AT STA 92.70 REQUIRES LOWER SKIN CUTOUT FOR ACCESS TO REPAIR THE #3 RIB STIFFENER. ER. REPEATINSPECTIONS EVERY 9,000 FLIGHT CYCLES THERE AFTER SEE PLISHED ON MAIN TASK (REFERENCE SUB TASK ST-001: PERFORMED 737 N 1-2R.REFERENCESDR CALA2022090702288None · noneL/H HORIZONTAL STAB LOWER SKIN REQUIRES CUTOUT AT STA. 92.70 #1 VERTICAL RIB STIFFENER REPAIR. 41437 ACCOMPLISHED TASKS AND PARTIAL WORK ACCOMPLISHED (HFEC INS TE JULY 6 2022 06:54. HFEC COMPLETED ON UPDATED ENTRY SUB TASK 0 T-76511 PO: 123199. 2.) 7075 T-62 PSDR CALA2022083102229Skin · noneR/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LSDR CALA2022082902203None · crackedRIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0SDR CALA2022082902202Web · crackedCENTER WING BOX REAR SPAR PRESSURE WEB ALONG VERTICAL PRESSURE DECK, AROUND RBL 33.5 APPROXIMANELY, WEB IS CRACKED. 1" CRACK AT RBL 33.5 AND A 1" CRACK AT RBL 40.0 REF. BAM N/R 000852241 AND 000852243. THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION. SDR CALA2022082402151Skin · damagedR/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LSDR CALA2022082402150Stabilizer · crackedRIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0SDR CALA2022081602096Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN - CRACK FOUND (2 IN LENGTH) BE TWEEN STAB STA 120.50 AND 129.50 AND 1 INCH FWD OF THE REAR SPAR . (6 INCHES FROM THE AFT INBOARD CORNER OF THE EXISTING REPAIR). REF NON-ROTUINE 000803467. EXISTING REPAIR DOUBLER AT STAB STA. 129SDR CALA2022081602095Skin · interferenceLH HORZ STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STIFFENER #1 CRACK REPAIR( N/R 000814111)AND N/R 000841437. THRESHOLD 56,000 FLIGHT CYCLES FOR A DETAIL VISUAL INSPECTION AN INSPECTIONS EVERY 9,000 FLIGHT CYCLES THERE AFTER SEE SRM 55-10- REFSDR CALA2022081602094Skin · interferenceLH HORZ STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STIFFENER #3 CRACK REPAIR( N/R 000841433)AND N/R 000841447. REPAIR DOUBLER INSTALLED ISSUED DIP TO READ " INSPECTION THRESS EXTERNAL (LFEC) INSPECTION OF REPAIR DOUBLER. REPEAT INSPECTIONS REPASDR CALA2019121602218Unknown · abnormalFWD CARGO PIT MAGIC CARPET DISCHARGING STATIC DURING OPERATION ACROSS FWD L/H EXTENSION ARM AND ROLLER GUIDE PANEL. INVESTIGATING AND CLEANED MOUNTING HARDWARE. UNKNOWN REASON FOR STATIC DISCHARGE. CONTACTED TECH SUPPORT. NEED MORE GROUND TIME TO TROUBLESHOOSDR CALA2017090803089Sign · looseEMERGENCY EXIT SIGN OVER THE WINDOW FOUND LOOSE. SECURED THE LIGHT.SDR CALA2017072802382Window · failedNO. 2 RIGHT WINDOW SHATTERED. FLAMES OBSERVED OUTSIDE WINDOW FRONT NEAR BOTTOM. POWER OFF EXT FIRE. REMOVED AND REPLACED R2 SLIDING WINDOW ASSY IAW AMM 56-12-11. OPS CHECKED GOOD.SDR CALA2017062301965Light · inoperativeEMERGENCY LIGHT OVERHEAD ROW 11ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW MM 33-51-03.SDR CALA2017020600269Power Supply · inoperativeEMERGENCY EXIT AREA LIGHT AT SEAT 14ABC AN D 21ABC ARE INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-51-06-960-806. OPS CHECKED GOOD.SDR CALA2017010600011Control Panel · faultyENG 1 OVERHEAT LIGHT IS ON ENG1 OVERHEAT ON CLIMB THROTTLE AT IDLE FOR AT LEAST 5 MINS BEFORE LIGHT WENT OUT SMOOTH. EMERGENCY DECLARED. CAPT REPORTED THAT EGT WAS NOT EXCEEDED NOR DID HE GET AN ENGINE FIRE INDICATION. ALL PARAMETERS WERE NORMAL. PERFORMED ENGSDR CALA2015072100591Structure · corrodedCORROSION FOUND ON LT CHORD 23L, SEVERAL SPOTS STATION 288 - 351. REPAIR PERFORMED IAW ECRA 5310-06549.SDR CALA2015072100590Gusset · corrodedCORROSION FOUND ON STRINGER 21 LT, BETWEEN STATION 297 - 308 ON GUSSET. REPAIR PERFORMED IAW ECRA 5310-0659.SDR CALA2015072100589Stringer · corrodedCORROSION FOUND ON STRINGER 25L AT STATION 360. REPAIR WORK COMPLETED IAW ECRA 5310-06551.SDR CALA2015071700578Frame · crackedLEFT CABIN FRAME 500J HAS CRACK INDICATION AT INBD RADIUS, NEAR INBD RIVET AT 4 O CLOCK POSITION. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER IAW ECRA 5310-0654 5. DIP INITIATED TO ACCOMPLISH REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL AIRFRAME FLSDR CALA2015071700576Frame · crackedMFEC FRAME STATION 400R BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV I, FOUND CRACK AT INBD FASTENER. PERFORMED INTERIM REPAIR IAW ECRA 5310-06540 PART 1 IAW STEP 16 OF PART 1.SDR CALA2015071700574Frame · crackedMFEC FRAME STATION 727B RT, BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV L, FOUND CRACK AT INBD FASTENER. REPAIRED RT FRAME IAW EA 5310-04716 REV L. SEE ALL WIPS & TASKS FOR WORK PERFORMED.SDR CALA2015071700573Frame · crackedLEFT CABIN FRAME 727B HAS CRACK INDICATION AT INBD RADIUS NEAR INBD RIVET, AT 4 O CLOCK POSITION. REPAIRED LT CABIN FRAME AT STATION 727B BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV L. SEE WIPS & TASKS FOR WORK PERFORMED.SDR CALA2015062900533Frame · crackedLEFT CABIN FRAME 500E HAS A CRACK AT INBD RADIUS NEAR INBD RIVET AT 4 O CLOCK POSITION, FRAME 500E BETWEEN STRINGER 8L & 9L. REPAIRED IAW EA 5310-04716 REV L OP 3.
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