N196FE
Service difficulty reports · 23
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 = 'N196FE' 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 = 'N196FE' 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 FDEA202506221281Landing Gear · malfunctionedON TEST FLIGHT 9045 AFTER HMV 1/ 2 OUT OF INDIANAPOLIS TEST FLIGHT CREW PERFORMED ALT GEAR EXTENSION CHECK, FIRST ATTEMPT FAILED. CREW DEBRIEFED THAT THEY PERFORMED A NORMAL GEAR EXTENSION-RETRACTION SUCCESSFULLY, TRIED ALT GEAR EXTENSION A SECOND TIME ASDR FDEA202506211024Floorbeam · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231PFF APPEARS TO HAVE A SPEED TAPE REPAIR, APPROXIMATELY STATION 654 96. REPAIRED FLOOR PANEL (PNL# 231PFF MPN: 143T5876-129) AT STA. 654 22 Ï¿½ 750 BETWEEN LBL54.75 AND LBL77.5 IN REF. TO 767 SRM 53-00-50-2R ANSDR FDEA202506211023Hydraulic Line · crossedPITCH ENHANCEMENT SYSTEM CHECK (PTU) FAILS. STAB DOES NOT MOVE WITH LEFT AND CENTER HYDRAULICS SHUT DOWN. POWER TRANSFER UNIT CURRENTLY INSTALLED ON A/C 196: MPN 518735 SN MX814569. WHEN A/C PRE-DOCKS WERE ACCOMPLISHED WIC 2902100-00-01 FAILED. FOUND HYDRAUSDR FDEA202506201015Closeout Panel · gougedDURING ADJUSMENT OF #8 TELESCOPING DUCT SEAL FOUND EDGE NICKED. REPAIRED RH WING # 8 SLAT LWR INBD CLOSE OUT PANEL O/B EDGE BETWEEN WS 456.48 - 464.48. IN REF. TO 767 SRM 57-43-01-2R FIG.201 SHEET:4, REPAIR:3, AND 767 SRM 51-70-08-0G PARA 5.G. THIS IS A MASDR FDEA202506180980Floorboard · damagedNR# 204: MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 221EFF DENTED, APPROXIMATELY STATION 400. GM44 FABRICATED NEW FLOORBOARD (PNL# 221EFF MPN: 141T5856-109) AT STA. 285-412 BETWEEN LBL 33 AND LBL 54.75 REF EA# H-5321-T0383793 P1 AND BOEING DRW# 141T5856-109 SDR FDEA202506170978Floorboard · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231PFF APPEARS TO HAVE A SPEED TAPE REPAIR, APPROXIMATELY STATION 654 96. GM59 REPAIRED FLOOR PANEL (PNL# 231PFF MPN: 143T5876-129) AT STA. 654 22 750 BETWEEN LBL54.75 AND LBL77.5 IN REF. TO 767 SRM 53-00-50-2R SDR FDEA202506140941Floorboard · damagedNR# 0202: MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222CFF HAS NUMEROUS NUMEROUS DENTS, APPROXIMATELY STATION 350. GM41 . FABRICATED NEW FLOOR PANEL (PNL# 222CFF MPN: 141T5856-116) AT STA. 285 412 BETWEEN RBL54.75 AND RBL77.5 IN REF. TO EA# H-5312-T03837SDR FDEA202506140940Floorboard · damagedNR# 0179: MAIN CARGO, FLOOR PANEL 242UFF HAS A PUNCTURE. FABRICATED NEW FLOOR PANEL (PNL# 242UFF MPN: 145T5876-112) AT STA. 984.95 1114.82 BETWEEN RBL74.5 AND RBL54.75 IN REF. TO EA# H-5312-T0383753 P1 AND BOEING DRW# 145T5876-112. THIS IS A MAJOR REPAIRSDR FDEA202506140939Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231DFF DENTED, APPROXIMATELY STATION 424. GM45 FABRIACTED NEW FLOORPANEL 231DFF MPN# 143T5875-9 LBL 54.75-LBL 77.5 STA 412-500 IN REF TO EA# H-5312-T0383753. THIS IS A MAJOR REPAIR SEE JPF FOR ALL WORKSTEPS ACCOMPLISDR FDEA202506140938Floorboard · dentedNR# 0164: MAIN DECK FLOOR PANEL 241AGF NEEDS TO BE REPAIRED FOR MULTIPLE DAMAGES. FABRICATED NEW FLOORPANEL (PNL# 241AGF MPN:141T5876-113) LBL 77.50 STA 984.50-1114.82 IN REF TO BOEING DWG 141T5876-113.THIS IS A MAJOR REPAIR. SEE JPF FOR ALL WORK STEPS ACCSDR FDEA202506130932Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 221CFF HAS NUMEROUS DENTS, APPROXIMATELY STATION 350. GM38 FABRICATED FLOOR PANEL 221CFF MPN# 141T5856-105 LBL 11- RBL11 STA. 285-412 IN REF TO BOEING DRWNG. 141T5856-105. THIS IS A MAJOR REPAIR. SEE JPF FOR ALL WORSDR FDEA202506130931Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231QFF APPEARS TO HAVE A SPEED TAPE REPAIR, APPROXIMATELY STATION 654 96. GM58 FABRIACTED NEW FLOOR PANEL 231QFF IN REF TO BOEING DWG 143T5876-19 LBL 77.5- LBL 81 STA 654 22 -654 96. THIS IS A MAJOR REPAIR SEE JPF FSDR FDEA202506110920Floorboard · wornMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251AFF DENTED, APPROXIMATELY STATION 1124. GM60 REPAIRED FLOOR PANEL 251AFF (MPN 146T5869-8) AT STA 1100 TO STA 1197 22, LBL11 TO RBL11 IN REF TO B767 SRM 53-00-50-2R FIG 201, REPAIR 1 SHEET 4. THIS IS A MAJOR REPAISDR FDEA202506110919Floor Panel · wornMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231AFF DENTED, APPROXIMATELY STATION 424. GM46 FABRICATED NEW FLOORPANEL 231AFF MPN:143T5875-5 RBL 11 - LBL 11, STATION 412- 434 IN REF TO BOEING DWG 143T5875-5. THIS IS A MAJOR REPAIR. REMOVED FLOOR PANEL 231 AFF SDR FDEA202506110918Floorboard · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222AFF HAS NUMEROUS DENTS, APPROXIMATELY STATION 350. GM39 FABRICATED FLOOR PANEL 222AFF MPN 141T5856-107 RBL 11- RBL 33 STATION 285- STATION 412 IN REF TO BOEING DRAWING 141T5856-107. THIS IS A MAJOR REPAIR. SEE JPSDR FDEA202506110917Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF HAS NUMEROUS DENTS, APPROXIMATELY STATION 350. GM40 FABRICATED NEW FLOORPANEL 222BFF MPN: 141T5856-106 RBL 33- RBL 54.75 STA 285-412 IN REF TO BOEING DWG 141T5856-106. THIS IS A MAJOR REPAIR. SEE JPF FOR ALL SDR FDEA202506090852Floor Panel · dentedMAIN DECK CARGO COMPARTMENT,FLOOR PANEL 221DFF HAS NUMEROUS DENTS, APPROXIMATELY STATION 350. FABRICATED NEW FLOOR PANEL 221DFF PER BOEING DWG# 141T5856-117 AND SRM 53-00-50-2R, FIG 201, SHEET 2.SDR FDEA202409171352Computer · inoperativeSTATUS MESSAGE EICAS DISAGREE. AMM: 31-41-02-4 REMOVED AND REPLACED LEFT EICAS COMPUTER IAW 767 AMM 31-41-02-4. SOFTWARE CORRECT AND TESTS NORMAL. OK FOR SERVICE. SEE WRI: 31-61/2491.SDR FDEA202306241091Bracket · crackedRH WING OUTBD LEADING EDGE, FUELING STATION DOOR HOLD-OPEN BRACKET AT INBD EDGE OF DOOR IS CRACKED REMOVED AND REPLACED BRACKET IAW BAC DWG 114T2450, SHEET 1, REVISION JSDR FDEA202306241090Panel · dentedRH WING LOWER O/B ACCESS PANEL 643BB IS DENTED ON LOWER SURFACE REPAIRED RH WING LOWER O/B ACCESS PANEL 643BB REMOVING DAMAGE ON LWR SURFACE, CLEANING, POTTING HOLE REPAIR, LAYING UP REPAIR DOUBLER AND CURED IAW B767 SRM 57- 20-01-2R FIG. 201 REP 7 AND SRM SDR FDEA202306231081Bracket · crackedR/W, I/B LEADING EDGE, LES 283, TORQUE TUBE SUPPORT BRACKET IS CRACKED REMOVED CRACKED TORQUE TUBE BRACKET ON RIGHT WING I/B LEADING EDGE LES 283 IAW FEDEX B767 SRM 51-40-02-0G AND REPLACED WITH NEW TORQUE TUBE BRACKET PN 256T2425-5, P.O 1060626.1 PER BOEISDR FDEA202304210735Flap · crackedL/H INBD ELEVATOR HAS DAMAGE ON THE UPPER SIDE. (MWT) SECOND LOCATION AT STA .125. REPAIRED LH IB ELEVATOR UPPER SKIN AT 63" AFT OF HINGE LINE AND 17" FROM IB EDGE OF PART. REF 767 SRM 55-20- 01-2R , 51-70-05-0G PAR 5C AND E.A. H-5520-T0374127 REV A P1. TSDR FDEA202304210734Flap · crackedL/H INBD ELEVATOR HAS DAMAGE ON THE UPPER SIDE. REPAIRED LH IB ELEVATOR UPPER SKIN AT 46" AFT OF HINGE LINE AND 17" FROM IB EDGE OF PART. REF 767 SRM 55-20- 01-2R , 51-70-05-0G PAR 5C AND E.A. H-5520-T0374127 REV A P1. THIS IS A MAJOR REPAIR.
Back to N196FE