N170FE
Service difficulty reports · 39
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 = 'N170FE' 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 = 'N170FE' 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 FDEA202610231674Floor Panel · puncturedPUNCTURE FLOOR PANEL 232MFF IN THE MAIN DECK CARGO COMPARTMENT (ONE LOCATION) FLOOR PANEL 232MFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPIRED IAW SRM 53-00- 50-2R PAR. 4-B FIG. 201 SHEET 2 REV. 96 AUG. 15/2026SDR FDEA202610231673Floor Panel · brokenBROKEN FIBERS OF THE TOP SKIN OF THE FLOOR PANEL 221DFF IN THE MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 221DFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00- 50-2R PAR.4-B FIG. 201 SHEET 2 REV 96 AUG 15/2026SDR FDEA202610231672Floor Panel · puncturedPUNCTURED FLOOR PANEL 241AFF IN THE MAIN DECK CARGO COMPARTMENT. (QTY 1) FLOOR PANEL 241AFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00- 50-2R PAR. 4-B FIG. 201 SHEET 2 REV. 96 AUG 15/2026SDR FDEA202610231671Floor Panel · puncturedPUNCTURE FLOOR PANEL 242HFF IN THE MAIN DECK CARGO COMPARTMENT, (QTY 1) FLOOR PANEL 242HFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00- 50-2R PAR. 4-B FIG. 201 SHEET 2 REV. 96 AUG. 15/2026SDR FDEA202610221664Floor Panel · puncturedPUNCTURED FLOOR PANEL 251SFF IN THE MAIN DECK CARGO COMPARTMENT (QTY 1) FLOOR PANEL 251SFF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV 96 AUG 15/2026SDR FDEA202610221663Floor Panel · puncturedPUNCTURED FLOOR PANEL 231JFF IN THE MAIN DECK CARGO COMPARTMENT (ONE LOCATION) FLOOR PANEL 231JFF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV 96 AUG 15-2026SDR FDEA202610221662Floor Panel · puncturedPUNCTURED FLOOR PANEL 252HFF IN THE MAIN DECK CARGO COMPARTMENT (TWO LOCATIONS) FLOOR PANEL 252HFF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV 96 AUG 15/2026SDR FDEA202610221661Floor Panel · damagedBROKEN FIBERS ON THE OUTER SKIN OF FLOOR PANEL 231DFF IN THE MAIN DECK CARGO COMPARTMENT.(TWO LOCATIONS) FLOOR PANEL 231DFF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 REV 96 AUG 15/2026SDR FDEA202610221660Floor Panel · puncturedPUNCTURED FLOOR PANEL 251AFF MAIN DECK CARGO COMPARTMENT (QTY 1) FLOOR PANEL 251AFF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4-B FIG 201 SHEET 2 REV 96 AUG 15/2026SDR FDEA202610221659Floor Panel · puncturedPUNCTURED FLOOR PANEL 251LFF IN THE MAIN DECK CARGO COMPARTMENT.(ONE LOCATION) FLOOR PANEL 251LFF, MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV 96 AUG 15/2026SDR FDEA202610201630Floor Panel · delaminatedPLIES DELAMINATED ON THE AFT RT EDGE OF FLOOR PANEL 241NFF, MAIN DECK CARGO BAY (ONE LOCATION). THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PARA 4-B, FIG 201, SHEET 2, REV 96. AUG 15/2026.SDR FDEA202610201629Floor Panel · delaminatedPLIES DELAMINATED ON THE FWD LT EDGE OF FLOOR PANEL 241YFA, IN THE MAIN DECK CARGO BAY (ONE LOCATION). THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PARA 4-B, FIG 201, SHEET 2, REV 96. AUG 15/2026.SDR FDEA202610201628Floor Panel · crackedCRACKED FIBERS ON THE OUTER SKIN OF FLOOR PANEL 241YFA IN MAIN DECK CARGO BAY (FOUR LOCATIONS). THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 96. AUG 15/2026.SDR FDEA202610201627Floor Panel · puncturedPUNCTURED FLOOR PANEL 241PFF IN THE MAIN DECK CARGO BAY (QTY 2). THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, REV 96.SDR FDEA202610201626Floor Panel · puncturedPUNCTURED FLOOR PANEL 241KFF IN THE MAIN DECK CARGO BAY (THREE LOCATIONS) THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 96. AUG 15/2026.SDR FDEA202610201609Floor Panel · crackedCRACKED FIBERS ON THE OUTER SKIN OF FLOOR PANEL 241ZFF IN THE MAIN DECK CARGO BAY (QTY 2). THE FLOOR PANEL 241ZFF WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4B, FIG 201, REV 96.SDR FDEA202610201608Floor Panel · crackedCRACKED FIBERS ON THE OUTER SKIN OF FLOOR PANEL 241AGF IN THE MAIN DECK CARGO BAY (QTY 2). THE FLOOR PANEL 241AGF WAS REPAIRED IAW SRM 53-00-50-2R, PARA 4B, FIG 201, REV 96.SDR FDEA202610201607Floor Panel · damagedBROKEN FIBERS ON THE OUTER SKIN OF FLOOR PANEL 242SFF IN THE MAIN DECK CARGO BAY. THE FLOOR PANEL 242SFF WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4B, FIG 201, REV 96.SDR FDEA202608041084Loop · inoperativeEVAS GLARESHIELD HOOK & LOOP ON LT & RT SIDE REQUIRES REPLACEMENT. HOOK & LOOP IS COMPLETELY WORN OUT. INSTALLED NEW HOOK & LOOP FOR BOTH CAPT'S AND F/O'S EVAS SYSTEMS IAW AMM 25-99-99-8-0 . OK FOR SERVICESDR FDEA202410191554Skin · wornLH WING SLAT 5, INNER SURFACE, BETWEEN WS 433.1 TO 460.2 WITH WEAR LH WING SLAT 5, INNER SURFACE, BETWEEN WS 433.1 TO 460.2 WAS REPAIRED IAW B767 SRM 57- 43-02-2R REP 1 (SHEET 1) FIG 201 AND SRM 51-70-10-2R FIG 208 SHEET 1 REV 90 AUG 15/2024SDR FDEA202410191553Slat · wornLH WING SLAT 5, BETWEEN WS 486.2 TO 512.2 WITH WEAR LH WING SLAT 5, BETWEEN WS 486.2 TO 512.2 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 (SHEET 1) FIG 201 AND SRM 51-70-10-2R FIG 208 SHEET 1 REV 90 AUG 15/2024SDR FDEA202410161529Skin · delaminatedLH WING, INBD FLAP (OUTBD SECTION), LEADING EDGE WITH DELAMINATION. LH WING INBD FLAP (OUTB SECTION) LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIGURE 201 (SHEET 2) AND (SHEET 5) TABLE 1 AND SRM 51-70-17-0G PAR 4.A FIGURE 10 (SHEET 1) REV SDR FDEA202410161528Skin · dentedRIGHT WING, INBOARD MAIN FLAP LOWER SURFACE WITH DENT AT 15" FROM OB FLAP SUPPORT AN 13" FROM LOWER EDGE RH WING INBOARD MAIN FLAP LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIGURE 201 (SHEET 2) NOTE "A" AND SRM 51-70-03-0G PAR 5.L FIGURESDR FDEA202410151513Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 241JFF ON MDC SECTION 45. FLOOR PANEL 241JFF MDC SECTION 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202410141501Floor Panel · dentedPUNCTURE ON FLOOR PANEL 231UFF UPPER SURFACE SECTION 43 OF MDC. FLOOR PANEL 231UFF SURFACE SECTION 43 WAS REPAIRED IAW B767 SRM 53-00-50-2R REV 90 AUG 15/2024SDR FDEA202410141500Floor Panel · dentedMISSING MATERIAL AND DENTS ON UPPER SURFACE FLOOR PANEL 222BFF SECTION 41 OF MDC. MAIN DECK CARGO FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024SDR FDEA202410141499Floor Panel · dentedMISSING MATERIAL AND DENTS ON UPPER SURFACE FLOOR PANEL 222CFF SECTION 41 OF MDC. MAIN DECK CARGO FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024SDR FDEA202410141498Floor Panel · dentedMISSING MATERIAL AND DENTS ON UPPER SURFACE FLOOR PANEL 222AFF SECTION 41 OF MDC. MAIN DECK CARGO FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024SDR FDEA202410141497Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241KFF UPPER SURFACE SECTION 45 OF MDC. FLOOR PANEL 241KFF UPPER SURFACE SECTION 45 OF MDC WAS REPAIRED IAW B767 SRM 53-00- 50-2R REV 90 AUG 15/2024SDR FDEA202410141496Floor Panel · dentedMISSING MATERIAL AND DENTS ON UPPER SURFACE FLOOR PANEL 221DFF SECTION 41 OF MDC. MAIN DECK CARGO FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024SDR FDEA202404110455Warning Message · illuminatedAFTER TOUCHDOWN GOT A R HYD PRIM PUMP EICAS, RAN QRH, CONTINUED TAXI, DURING TAXI GOT A R HYD SYS PRESS EICAS, RAN QRH LOST SOME BRAKING, SO ELECTED TO GET TOW IN GATE. SHGN 10APR24 17:37 MEM AMM: 29_11_00_2_0 VERVIFIED AT RIGHT SYSTEM HYD RESERVOISDR FDEA202206041376Former · crackedCRACKED FORMER 114T2170-5 WITH LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441. 0000553921 : DAVIES, ANDREW M - 04-JUN-2022 22:16 REMOVED AND REPLACED CRACKED FORMER, LOOSE AND MISSING FASTENERS PER E.A, H-5720-T0368803 P1SDR FDEA202012093079Former · crackedLT WING LEADING EDGE, FORM P/N 114T2170-5 CRACKED AT OUTBOARD SIDE OF THE INBOARD AUX TRACK OF THE NR 5 SLAT BETWEEN WS 433 AND 460, STREAMER ATTACHED. REMOVED AND REPLACED NOSE FORMER PN 114T2127-4 ON LT WING STA OSS441, PER FEDEX EA: H-5720-T0358462-P1. TISDR FDEA202012083074Former · crackedLT WING LEADING EDGE 1 EACH FORM CRACKED AT THE OUTBOARD SIDE OF ROTARY ACTUATOR OF THE NR 5 SLAT BETWEEN WS 486.2 AND 512.2 STREAMER ATTACHED. REMOVED AND REPLACED NOSE FORMER AT OSS 499, PER BAC DWG 114T2161 REV B FEDEX B767 SRM 51-40-02 AND FEDEX EA H-5720SDR FDEA202012083073Former · crackedLT WING LEADING EDGE FORM P/N 114T2170-3 CRACKED AT INBOARD SIDE OF INBOARD AUX TRACK OF NR 5 SLAT BETWEEN WS 433 AND 460. STREAMER ATTACHED FABRICATED FORMER LT WING LEADING EDGE PN 114T2170-3 AT INBOARD SIDE OF INBOARD AUX TRACK, IAW BAC DWG 114T2170. INSTSDR FDEA202012083069Skin · delaminatedRIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE IS DELAMINATED 2" FORWARD OF TRAILING EDGE AND 7" INBOARD OF THE OUTBOARD EDGE. REPAIRED RIGHT WING INBOARD TRAILING EDGE AFT FLAP LOWER SURFACE, IAW B767 SRM 57-53-01-2R FIGURE 201 DETAIL 3, 51-70-10-2R REPSDR FDEA202012033020Bracket · crackedLT WING INBOARD FIXED LEADING EDGE, 1 EACH TORQUE TUBE BRACKET CRACKED APPROXIMATELY LES 285. STREAMER ATTACHED, REMOVED AND REPLACED BRACKET, IAW BAC DWG 114T1240 REV E AND B767 SRM 51--40-02.SDR FDEA202012013025Attach Angle · crackedNR 1 PYLON AFT FAIRING, OUTBOARD FRAME ATTACH CLIP IS CRACKED AT NAC STA 376 LT. REMOVED AND REPLACED CLIP, IAW B767 SRM 51-40-02.SDR FDEA202011293053Frame · crackedNR 2 PYLON CENTER FITTING AT STA 329 INBOARD SIDE CRACKED. ACCOMPLISHED FRAME CRACK REPAIR AT NAC 329, IAW B767 SRM 54-52-71-2R.
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