N127FE
Service difficulty reports · 35
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 = 'N127FE' 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 = 'N127FE' 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 FDEA202506261061Web · crackedMEC, LT TUNNEL, STA 246 - STA 266 FLOORBEAM WEB CRACKED, LBL APPROX 48 FABRICATED/REPLACED WEB P/N 141T5602-2, REF B767 SRM 51-40-02-0G & BOEING DRW 141T5602.THIS IS A MAJOR REPAIRSDR FDEA202506251048Floorboard · damagedNR# 0293: MAIN CARGO DECK, FLOOR PANEL 242JFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 242JFF, MPN:145T5876-102, RBL 33 - RBL 11, STA. 930 Ï¿½ 984.95 IN REF TO BOEING DWG# 145T5876-102. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATIONSDR FDEA202506251046Floorboard · damagedNR# 0297: MAIN CARGO COMPARTMENT, FLOOR PANEL 242SFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 242SFF, MPN:145T5876-104, RBL 33- RBL 11, STATION 984.95 - 1114.82 IN REF TO BOEING DWG 145T5876-104. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSDR FDEA202506241040Floorboard · damagedNR# 0296: MAIN CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 241WFF, MPN:145T5876-51, RBL 11- LBL 11, STATION 984.95 - 1114.82 IN REF TO BOEING DWG 145T5876-51. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSSDR FDEA202506241039Floor Panel · damagedMAIN CARGO COMPARTMENT, FLOOR PANEL 242LFA HAS DAMAGE. FABRICATED MAIN COMPARTMENT, FLOOR PANEL 242LFA (MPN: 145T5876-110) AT STA 930 TO STA 984, RBL 54.75 TO RBL 74.25 IN REF TO BOEING DRAWING 145T5876 ID# 110.THIS IS A MAJOR REPAIR. PLEASE SEE SEQ CARD 1SDR FDEA202506241037Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS DAMAGE : CORRECTION FLOOR PANEL 242UFF FABRICATED FLOORPANEL 242UFF MPN# 114T5876-112 STA: 980-1114.82 RBL: 54.75- RBL 74.25 IN REF TO BOEING DRAWING 114T5876-112. SEE JPF FOR ALL WORK STEPS ACCOMPLISHED. THISSDR FDEA202506221025Floor Panel · wornMAIN CARGO COMPARTMENT, FLOOR PANEL 241LFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 241LFF, MPN:145T5876-19, RBL 11 LBL 11, STATION 930-984.95 IN REF TO BOEING DWG 145T5876-19. SEE JPF FOR ALL WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANSDR FDEA202503050334Windshield · crackedDURING CRUISE AT FL320, CAPTAIN S WINDSHIELD CRACKED IN A SPIDER WEB DESIGN. L FWD WINDSHIELD HEAT WENT INOP. WINDSHIELD REMOVED. WINDSHIELD HARDWARE IN FLIGHT DECK. J1 / J15 PINS REMOVED. INSTALLATION COMPLIED WITH FROM PARA G (18) IAW AMM 56-11-01-4. SYSDR FDEA202412241829Former · crackedRIGHT WING LEADING EDGE FORMER AT STA 433 CRACKED. REMOVED AND REPLACED RIGHT WING LEADING EDGE FORMER AT STA 433 REF 57-41-01-2RSDR FDEA202410151502Control Unit · failedMAIN CARGO DOOR LIGHT EICAS AND CARGO DOORS DISCREET LIGHT CAME ON DURING FLIGHT. 3 LIGHTS ON MAIN ENTRANCE DOOR PANEL WERE EXTINGUISHED. EXECUTED QRH PROCEDURES. REMOVED & REPLACED THE PSEU PER THE ABOVE AMM REFERENCE, ALL TESTS PASS.SDR FDEA202409011212Retainer · crackedLOWER FORWARD CARGO DOOR SEAL RETAINER DAMAGED AT UPPER FORWARD AREA. LWR FWD CGO DOOR, UPPER SEAL RETAINER REPAIR PERFORMED IAW B767 SRM 52-30-02-2R REPAIR 5. MAJOR REPAIR. SEE JPF.SDR FDEA202306291126Slat · damagedPERFORM MAJOR REPAIR TO SLAT #11 TRAILING EDGE WEDGE IN ACCORDANCE WITH 51-70-10-2R IN THE AREA OF SLAT #11 OSS 933.729. REF B767 SRM51-70-10-2R REPAIR4 & EA:H-5750-T0369144 P3 REPAIR THE #11 SLAT TRAILING EDGE WEDGE AT OSS 933.729. EA TITLE: WINGS - RHSDR FDEA202210222644Former · crackedL/WING FLE OSS 499 HAS A CRACKED FORMER REPLACED FORMER B67-57-002-03 AT L/WING FLE OSS 499 USING EA H-5720-T0371261 AS REFERENCE.SDR FDEA202206231539Slat · chafedRH WING LEADING EDGE SLAT #11 HAS A WEAR GROOVE ON THE UNDERSIDE(CONCAVE SIDE) SKIN. COMPLIED WITH E.A. H-5750-T0369144 P1.SDR FDEA202009162253Floor Panel · delaminatedMAIN CARGO FLOOR PANEL 242TFA DELAMINATED AND HAS EDGE DAMAGE AT CORNER. REPAIRED AREAS OF DELAMINATION AND EDGE DAMAGE TO CARGO FLOOR PANEL 242TFA, IAW B767 SRM 53-00-50-2R.SDR FDEA202009162226Angle · crackedNR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH ANGLE CRACKED AT NAC STA 295 LT. REMOVED AND REPLACED ANGLE, PER B767 SRM 551-40-02 AND BOEING DWG 313T3310 REV B.SDR FDEA202009152221Housing · crackedAFT CARGO DOOR UPPER AFT CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER AFT CARGO LIGHT, IAW B767-AMM 25-00-00-8.SDR FDEA202009152220Housing · crackedAFT CARGO DOOR UPPER FWD CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER FWD CARGO LIGHT, IAW B767-AMM 25-00-00-8.SDR FDEA2020091432191Skin · chafedRIGHT WING SLAT NR 11, T/E LOWER SURFACE CHAFE AT O/B TRACK. REPAIRED RT WING NR 11 SLAT T/E LOWER SURFACE CHAFE AT O/B TRACK WITH 250 DEG METAL BOND, IAW B767 SRM 57-43-01-01 FIG 1 DETAIL NR 1, 57-43-02-01 FIG 1 DETAIL NR 4, 57-43-02-2R REPAIR 1 DETAIL NR SDR FDEA2020091422186Beam · gougedNR 2 PYLON AFT FAIRING INBOARD LONGITUDINAL BEAM GOUGED AT NUTPLATE LOCATION AT NAC STA 308 LT. REMOVED LATCH BEAM, IAW B767 SRM 51-40-02-0G. REPAIRED LATCH BEAM, IAW B767 SRM 54-52-71-2R AND FED EX EA H5450-T0356442 P1. REINSTALLED LATCH BEAM, IAW B767 SRMSDR FDEA202009112171Floor Panel · damagedMAIN CABIN FLOOR PANEL 242GFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 242GFF, IAW B767 SRM 53-00-50-2R.SDR FDEA202009112170Floor Panel · damagedMAIN CABIN FLOOR PANEL 241ZFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R.SDR FDEA2020090982147Former · crackedRT WING LEADING EDGE INTERNAL FORMER CRACKED ON OUTBOARD SIDE OF SLAT NR 8 OUTBOARD ACTUATOR. REMOVED AND REPLACED RT WING RIB FORMER AT W/S 480, PER FEDEX B767 SRM 51-40-02 & BAC DWG 114T2511. LOCATED AND DRILLED PER FEDEX B767-SRM 51-40-05.SDR FDEA2020090972139Bracket · crackedLT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED, LEADING EDGE STA 430. REMOVED CRACKED FORMER BRACKET IAW B767 SRM 51-40-02, MATERIAL ID 2024T3 .040" IAW BAC DWG 114T2170. FABRICATED RIB FORMER BRACKET, IAW BOEING DWG 114T2170 REV ALODINED, IAW BOEINSDR FDEA2020090972138Splice Plate · crackedRT WING LEADING EDGE INTERNAL SPLICE PLATE CRACKED APPROX 1' OUTBOARD OF SLAT #8 OUTBOARD ACTUATOR. REMOVED AND REPLACED SPLICE P/N 114T2800-165, PER BAC DWG 114T2800 REV G.SDR FDEA2020090972137Bracket · crackedLT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED. LEADING EDGE STA 480 REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2511, REV D, B767 SRM 51-40-02 AND B767 SRN 51-40-03.SDR FDEA2020090962134Bracket · crackedLEFT WING PANEL 511KB AREA INBOARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET P/N 256T2425-6, PER BOEING DWG 114T1240 REV D.SDR FDEA2020090942107Bracket · crackedRT WING PANEL 611KB AREA IB BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON RT WING PANEL 611KB AREA, PER FEDEX B767 SRM 51-40-02 AND PER BOEING DWG 114T1240 REV D.SDR FDEA2020090922082Former · crackedLT WING LEADING EDGE CAVITY FWD FORMER STRAP CRACKED LEADING EDGE STA 505. REMOVED AND REPLACED LT WING LEADING EDGE CAVITY FWD FORMER STRAP LES 505 PN 114T2800-165 SEAL STRIP PO NR 979532.1, IAW BAC DWG 114T2800 REV G, B767 SRM 51-40-02.SDR FDEA202006261369Unknown · odorON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. PERFORMED AIR CONDITIONING OIL/FUME CONTAMINATION REMOVAL AS PER MM 21-00-21-2. OIL SMELL WITH PACKS RUNING HAS DISSIPATED, NO SMOKE OR FUMES. PERFORMED BOROSCOPE UNDER WRI 72-00/4125 AND MTSI 72-30/4072SDR FDEA202006261368Module · odorON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. REMOVED AND REPLACED YSM, PER AMM 27-09-00-2. CHECKS GOOD. UNIT CHANGED, YAW DAMPER/STAB TRIM MODULE.SDR FDEA201909112212Pressure Switch · failedUNSCHD STAB TRIM FOR APPROXIMATELY 2 SECONDS ON EICAS, PASSING 8000 FT DURING DESCENT SPEED 210 KTS FLAP 1. REPLD C HYD PRESS SWITCH S29. PRESSURE SWITCH LEAK CKS GOOD. PERFORMED OPS CK OF ADP REF AMM 29-11-03-4-0. T/S UNSCHED STAB TRIM REF FIM 27-09 FAULT TRESDR FDEA2018110213074Escape Rope · unsecureON ARRIVAL AT THE ACFT, FOUND AN ESCAPE ROPE DROPPED DOWN AT THE FRONT OF DOOR. RESTORED THE L1 ENTRY DOOR ESCAPE ROPE IAW MM 25-61-04-2-1. AIRCRAFT OK SERVICE.SDR FDEA201802110336Transmitter · malfunctionedRECEIVED RED STABLIZER WARNING ON INITIAL POWER APPLICATION DURING PREFLIGHT STAB TRIM SET TO 6.75. CONFIG T/O CHECK PERFORMED 3 TIMES. AFTER WARNING, STAB INDICATED (AN UNCOMMANDED MOVE) TO 7.1 OR 7.2. CONCLUDED WE HAD UNCOMMANDED MOVEMENT OF APPROX 1/3 UNISDR FDEA201606152003Rotary Actuator · inoperativeAT 220 KTS RECEIVED L/E SLAT DISAGREE LIGHT. ACCOMPLISHED QRH CHECKLIST 9.1.10, L/E SLAT DISAGREE 0. L/E WOULD NOT DEPLOY BEYOND, BETWEEN UP AND 1, USING ALT FLAPS. QRH LEAD ME TO RUN QRH 9.1.6, L/E SLAT ASYM CHECKLIST. FLAPS DEPLOYED TO 20 USING ALT FLAPS
Back to N127FE