N161FE
Service difficulty reports · 43
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 = 'N161FE' 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 = 'N161FE' 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 FDEA202601080014Skin · dentedRIGHT INBD TE FLAP AFT FLAP IS DAMAGED ON THE UPPER SURFACE. REPAIRED RT INBD TE FLAP AFT FLAP TOP UPPER SURFACE AT WS STA. 287.4 IAW SRM 57-53-01-2R, FIG 201, SHEET 4, REPAIR 1, & SRM 51-70- 10-2R. MAJOR REPAIR. SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.SDR FDEA202601080012Floor Panel · damagedMAIN CARGO FLOOR PANEL 242VFF HAS DAMAGE MARKED IN RED. FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5876-114, RBL 74.25- RBL 86.25, STA 984.95-1087 IN REF. TO BOEING DWG 145T5876-114. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATIONSDR FDEA202404300524Engine · failedCLIMBING THRU FL330, LEFT ENGINE OIL PRESSURE DROPPED TO 1 PSI. EICAS RED BOX, L ENG OIL PRESS, AND A BUMP FELT. RAN QRH, EVENTUALLY SHUT DOWN ENGINE, DECLARED EMERGENCY, RETURNED TO INDY. OIL TEMP DROPPED FROM ~115 TO 85. EMERGENCY DECLARED. PER THE DFSDR FDEA202403200322Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222CFF SECTION 41. FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202403200321Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 221CFF SECTION 41. FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202403200320Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 221DFF SECTION 41. FLOOR PANEL 221DFF SECTION 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202403200319Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF SECTION 41. FLOOR PANEL 222BFF SECTION 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202403200318Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222AFF SECTION 41. FLOOR PANEL 222AFF SECTION 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202208031853Lamp · inoperativeNO NOSE GEAR INDICATION ON EXTENSION. NO DISAGREE INDICATION HYDRAULICS NORMAL. NO GEAR OR DOOR LIGHTS ILLUMINATED. LANDED SAFELY EWR. ***EMERGENCY DECLARED*** REPLACED BOTH NOSE GEAR INDICATION LAMPS PER 767 AMM 33-16-02-2. OPS CHECKS GOOD. A/C OK SDR FDEA202208031851Lamp · inoperativeNO NOSE GEAR INDICATION ON EXTENSION. NO DISAGREE INDICATION HYDRAULICS NORMAL. NO GEAR OR DOOR LIGHTS ILLUMINATED. LANDED SAFELY EWR. ***EMERGENCY DECLARED*** NOSE GEAR LIGHT ASSY. REPLACED BOTH NOSE GEAR INDICATION LAMPS IAW AMM 33-16-02-2. OPS CHESDR FDEA202204110923Former · crackedRIGHT WING FIXED L/E AREA, FORMER CRACKED AT BULLNOSE AREA OF THE L/E AT RIB #13 (COUNTING FROM I/B TO O/B) APPROX L/E STA. 490. REMOVED AND REPLACED THE OUTBD RIGHT WING FIXED L/E NOSE FORMER AND ATTACH ANGLE AT OSS 499 IAW BAC DWG 114T2161, REV. - AND FESDR FDEA202204110922Former · crackedRIGHT WING FIXED L/E AREA, FORMER HAS CRACK INDICATION AT THE I/B MAIN TRACK OF #9 SLAT APPROX. L/E STA. 562. REMOVED AND REPLACED THE OUTBD RIGHT WING FIXED L/E NOSE FORMER AND ATTACH ANGLE AT OSS 565 IAW BAC DWG 114T2162, REV. - AND FEDEX EA H-5720-T0367SDR FDEA202204110921Former · crackedLH WING OUTB FIXED LEADING EDGE FORMER IS CRACKED AT RIB #13 (MARKED) REMOVED AND REPLACED THE LEFT WING OUTBD FIXED L/E NOSE FORMER AND ATTACH ANGLE AT OSS 499 IAW BAC DWG 114T2161, REV. - AND FEDEX EA H-5720-T0367791-P1, TITLE: WING-SECONDARY WING STRCT SDR FDEA202204110920Angle · crackedLH WING OUTBD FIXED LEADING EDGE FORMER ATTACH ANGLE IS CRACKED AT LOWER FASTENER HOLE AT RIB #6 (MARKED) REMOVED AND REPLACED THE LEFT WING OUTBD FIXED L/E NOSE FORMER AND ATTACH ANGLE AT OSS 441 IAW BAC DWG 114T2241, REV. - AND FEDEX EA H-5720-T0367791-PSDR FDEA202204110919Beam · crackedRIGHT WING, LOWER TRAILING EDGE PANEL @ WS 685, AFT U-CHANNEL IS CRACKED IN SEVERAL PLACES REMOVED & REPLACED TRAILING EDGE PANEL SUPPORT BEAM IAW BAC DWG 113T1681 REVISION A & B767 AMM 20-11-00-2SDR FDEA202204080895None · crackedRW LWR T/E PANEL AT WS 685 ATTACH ROD AFT ATTACH BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 113T1681 SHEET 3, REVISION A, AND FEDEX EA H-5720-T0367856-P1 RELEASED APR 05, 2022, TITLED "WING - SECONDARY WING STRCT - RH WING, LOWER TRAILING EDSDR FDEA202204060882None · gougedLEFT WING #6 SPOILER LOWER SURFACE HAS HOLE APROXIMATELY 1"X1". ACCOMPLISHED PERMANET REPAIR OF PUNCTURE ON L/W #6 SPOILER LOWER SURFACE IAW FEDEX B767 SRM 57-70-01-2RFIG 201 SHEET 4 AND 51-70-05-2RSDR FDEA202204060881None · gougedRIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE IS GOUGED IB OF IB MAIN TRACK. REPAIRED RIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE GOUGE I/B OF I/B MAIN TRACK IAW B767-SRM-57-43-02-2R REPAIR 1 FIG 201 SHEET 1 AND 2.SDR FDEA202204060877Bracket · cracked#1 ENGINE PYLON, OTBD SIDE DRAIN TUBE ATTACH BRACKET IS CRACKED JUST BELOW PANEL 437BL CRACKED BRACKET ON #1 ENGINE PYLON, OUTBD DRAIN TUBE REMOVED & REPLACED WITH NEW BRACKET IAW BAC DWG 313T2380, REV-SDR FDEA202204050851Frame · cracked#2 PYLON, 447BR, HYDRAULIC BAY, MID FRAME IS CRACKED REPAIRED MID-SPAR FRAME IAW FEDEX EA H-5450-T0367830-P1, RELEASED APR04, 2022, TITLED "NACELLES / PYLON - WING PYLON / STRUT - #2 PYLON, NAC STA 329, FAIRING, FRAME, SRM REPAIR DEVIATIONSDR FDEA202204050850Frame · cracked#1 ENGINE, INBD SIDE, MID PYLON FRAME UNDER THE LATCH BEAM IS CRACKED REPAIRED MID-SPAR FRAME IAW FEDEX EA H-5450-T0367836-P1, RELEASED APR 04, 2022, TITLED " NACELLES / PYLON - WING PYLON / STRUT - #1 PYLON, NAC STA 329, FAIRING, FRAME, SRM REPAIR DEVIATSDR FDEA202204040836Floor Support · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR, , SUPPORT STRUCTURE SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX LBL80 REMOVED AND REPLACED CRACKED SPLICE ANGLE WITH NEW ANGLE IAW BAC DWG 146T5650, REV. CSDR FDEA202204040832Skin · gougedRIGHT WING #8 SLAT LOWER TRAILING EDGE AFT WEDGE IS GOUGED OB OF MAIN TRACK. REPAIRED GOUGE ON R/W #8 SLAT T/E WEDGE LOWER SKIN AT O/B OF MAIN TRACK WITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR1 SHEET 1, 51- 70-10-2R REPAIRSDR FDEA202204030826Floor Support · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR SUPPORT STRUCTURE, OTBD SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX LBL82 REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW B767 SRM 51-40-02-0G AND BAC DWG 146T5650, REV. C.SDR FDEA202204030825Skin · gougedRIGHT WING #8 SLAT LOWER TRAILING EDGE AFT WEDGE IS GOUGED OB OF IB AUX TRACK. REPAIRED GOUGE ON R/W #8 SLAT T/E WEDGE LOWER SKIN AT O/B OF I/B AUX TRACKWITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR 1 SHEET 1, 51- 70-10-2R, SDR FDEA202204030824Skin · gougedLW #5 SLAT INBD T/E LWR SURFACE IS GOUGED. REPAIRED GOUGE ON L/W #5 SLAT T/E LOWER SURFACE WITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR 1 SHEET 1, 51-70-10-2R, 57-43-01- 0I, 51-20-05 AND B767 AMM 51-21-01/701, B767 NDTM PARSDR FDEA202204030822Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 242HFF HAS A PUNCTURE, STA 889 AND RBL 78 REPAIRED PUNCTURE ON MAIN CABIN FLOOR PANEL 242HFF IAW B767 53-00-50-2R, PARA. 4.C.SDR FDEA202204030821Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 241ZFF HAS DAMAGE, STA 1105 AND LBL 71 REPAIRED PUNCTURE ON MAIN CABIN FLOOR PANEL 241ZFF IAW B767 SRM 53-00-50-2R, PARA. 4.C.SDR FDEA202204030820Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 241WFF HAS SEVERAL AREAS OF DAMAGE, STA 1041 AND BL-0 REPAIRED 8EA DAMAGE LOCATIONS ON MAIN CABIN FLOOR PANEL 241WFF IAW B767 SRM 53-00- 50-2R, PARA. 4.C. AND 4.D.SDR FDEA202204030819Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 242VFF HAS DAMAGE AT STA 1012 AND RBL 79 REPAIRED PUNCTURE ON MAIN CABIN FLOOR PANEL 242VFF IAW B767 SRM 53-00-50-2R, PARA. 4.C.SDR FDEA202204030818Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 241KFF HAS 2 AREAS OF DAMAGE REPAIRED 2EA AREAS OF DAMAGE ON MAIN CABIN FLOOR PANEL 241KFF IAW B767 SRM 53-00- 50-2R, PARA. 4.C.SDR FDEA202204010809Strap · crackedRIGHT WING FIXED LEADING EDGE AREA, BULL NOSE STRAP IS CRACKED APPROX L/E STA 503 REMOVED & REPLACED STRAP IAW BAC DWG 114T2800, SHEET 5, REVISION GSDR FDEA202203300765Angle · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR SUPPORT STRUCTURE SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX. RBL 80. REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW BAC DWG 146T5650, REV. C.SDR FDEA202203300762None · cracked#2 PYLON, AREA AFT OF HYDRAULIC BAY, INBOARD SIDE, SUPPORT BRACKET IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T2303, SHEET 166, REVISION -SDR FDEA202203300761Shear Tie · cracked#1 ENGINE PYLON, INBOARD SIDE, INTERNAL SHEAR TIE IS CRACKED JUST FWD OF PANEL 437BR REMOVED & REPLACED SHEAR TIE @ #1 ENGINE PYLON, INBOARD SIDE, INTERNAL JUST FWD OF PANEL 437BR IAW BAC DWG 313T3310SHEET 95, REVISION - & B767 SRM 51-40-02-0GSDR FDEA202202290739Bracket · crackedRIGHT WING LEADING EDGE TORQUE TUBE SUPPORT BRACKET IS CRACKED AFT OF # 7 SLAT OUTBOARD SIDE AT LES 283.82 REMOVED & REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 114T1240 REVISION ESDR FDEA202008021753Charger · malfunctionedMAIN BATTERY CHARGER STATUS MESSAGE IN-FLIGHT AFTER 1 20 TIME ENROUTE. T.T. RMV AND REPLACED MAIN BATTERY CHARGER, REF AMM 24-31-02-4 AND MAIN BATTERY, REF AMM 24-31-01-04. BOTH OPERATIONS CHECK GOOD STATUS MESSAGE CLEARED.SDR FDEA2020080321753Charger · failedMAIN BATTERY CHARGER STATUS MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE MAIN BATTERY CHARGER IAW AMM 24-31-02-4, AND AMM 24-31-01-04. BOTH OPS CHECKED GOOD STATUS MESSAGE CLEARED.SDR FDEA202004300857Skin · delaminatedRUDDER LOWER STATIC WICK MOUNT PLATE FWD END PULLED AWAY AND RUDDER SU SURFACE DISBONED. AREA 3 IN ABOVE WICK ALONG TRAILING EDGE HAS FRAYED EXPOSED C COMPOSITE (POSSIBLE LIGHTNING STRIKE) REPAIRED RUDDER IAW FEDEX EXPRESS EA# H-5540-T0353813 TITLE: STASDR FDEA202004270799Support Bracket · crackedRIGHT WING L/E CAVITY CURTAIN SUPPORT BRACKET CRACKED @ LE STA. 560 REMOVED AND REPLACED SUPPORT BRACKET IAW BAC DWG 114T2170 REV- AND B767 SRM 51- 40- 02SDR FDEA202004270798Support Bracket · crackedRIGHT WING L/E CAVITY CURTAIN SUPPORT BRACKET CRACKED @ LE. STA 490 REMOVED AND REPLACED SUPPORT BRACKET IAW BAC DWG 114T2170 REV- AND B767 SRM 51- 40-02SDR FDEA202004270797Support Bracket · crackedRIGHT WING L/E CAVITY CURTAIN SUPPORT BRACKET CRACKED @ LE.STA 433 REMOVED AND REPLACED SUPPORT BRACKET IAW BAC DWG 114T2170 REV- AND B767 SRM 51- 40-02.SDR FDEA202004270796Support Bracket · crackedRIGHT WING L/E CAVITY CURTAIN SUPPORT BRACKET CRACKED @ LE.STA 433 REMOVED AND REPLACED SUPPORT BRACKET IAW BAC DWG 114T2170 REV.- AND B767 SRM 51- 40-02
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