# Service difficulty reports: N170FE

A list on [N170FE](https://openairdocs.org/aircraft/N170FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202610231674](https://openairdocs.org/sdr/FDEA202610231674.md): Floor Panel · punctured · Oct 23, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE 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. 15/2026
- [SDR FDEA202610231673](https://openairdocs.org/sdr/FDEA202610231673.md): Floor Panel · broken · Oct 23, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > BROKEN 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 15/2026
- [SDR FDEA202610231672](https://openairdocs.org/sdr/FDEA202610231672.md): Floor Panel · punctured · Oct 23, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15/2026
- [SDR FDEA202610231671](https://openairdocs.org/sdr/FDEA202610231671.md): Floor Panel · punctured · Oct 23, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE 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. 15/2026
- [SDR FDEA202610221664](https://openairdocs.org/sdr/FDEA202610221664.md): Floor Panel · punctured · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15/2026
- [SDR FDEA202610221663](https://openairdocs.org/sdr/FDEA202610221663.md): Floor Panel · punctured · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15-2026
- [SDR FDEA202610221662](https://openairdocs.org/sdr/FDEA202610221662.md): Floor Panel · punctured · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15/2026
- [SDR FDEA202610221661](https://openairdocs.org/sdr/FDEA202610221661.md): Floor Panel · damaged · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > BROKEN 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 15/2026
- [SDR FDEA202610221660](https://openairdocs.org/sdr/FDEA202610221660.md): Floor Panel · punctured · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15/2026
- [SDR FDEA202610221659](https://openairdocs.org/sdr/FDEA202610221659.md): Floor Panel · punctured · Oct 22, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 15/2026
- [SDR FDEA202610201630](https://openairdocs.org/sdr/FDEA202610201630.md): Floor Panel · delaminated · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PLIES 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 FDEA202610201629](https://openairdocs.org/sdr/FDEA202610201629.md): Floor Panel · delaminated · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PLIES 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 FDEA202610201628](https://openairdocs.org/sdr/FDEA202610201628.md): Floor Panel · cracked · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > CRACKED 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 FDEA202610201627](https://openairdocs.org/sdr/FDEA202610201627.md): Floor Panel · punctured · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 FDEA202610201626](https://openairdocs.org/sdr/FDEA202610201626.md): Floor Panel · punctured · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURED 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 FDEA202610201609](https://openairdocs.org/sdr/FDEA202610201609.md): Floor Panel · cracked · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > CRACKED 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 FDEA202610201608](https://openairdocs.org/sdr/FDEA202610201608.md): Floor Panel · cracked · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > CRACKED 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 FDEA202610201607](https://openairdocs.org/sdr/FDEA202610201607.md): Floor Panel · damaged · Oct 20, 2026 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > BROKEN 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 FDEA202608041084](https://openairdocs.org/sdr/FDEA202608041084.md): Loop · inoperative · Aug 4, 2026 · N170FE · Boeing 767300 · Emergency Equipment
  > EVAS 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 SERVICE
- [SDR FDEA202410191554](https://openairdocs.org/sdr/FDEA202410191554.md): Skin · worn · Oct 19, 2024 · N170FE · Boeing 7673S2F · Leading Edge Devices
  > LH 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 15/2024
- [SDR FDEA202410191553](https://openairdocs.org/sdr/FDEA202410191553.md): Slat · worn · Oct 19, 2024 · N170FE · Boeing 7673S2F · Leading Edge Devices
  > LH 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 15/2024
- [SDR FDEA202410161529](https://openairdocs.org/sdr/FDEA202410161529.md): Skin · delaminated · Oct 16, 2024 · N170FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH 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 FDEA202410161528](https://openairdocs.org/sdr/FDEA202410161528.md): Skin · dented · Oct 16, 2024 · N170FE · Boeing 7673S2F · Trailing Edge Flaps
  > RIGHT 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 FIGURE
- [SDR FDEA202410151513](https://openairdocs.org/sdr/FDEA202410151513.md): Floor Panel · cracked · Oct 15, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > CRACK 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 15/2024
- [SDR FDEA202410141501](https://openairdocs.org/sdr/FDEA202410141501.md): Floor Panel · dented · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE 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 15/2024
- [SDR FDEA202410141500](https://openairdocs.org/sdr/FDEA202410141500.md): Floor Panel · dented · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > MISSING 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 15/2024
- [SDR FDEA202410141499](https://openairdocs.org/sdr/FDEA202410141499.md): Floor Panel · dented · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > MISSING 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 15/2024
- [SDR FDEA202410141498](https://openairdocs.org/sdr/FDEA202410141498.md): Floor Panel · dented · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > MISSING 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 15/2024
- [SDR FDEA202410141497](https://openairdocs.org/sdr/FDEA202410141497.md): Floor Panel · punctured · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE 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 15/2024
- [SDR FDEA202410141496](https://openairdocs.org/sdr/FDEA202410141496.md): Floor Panel · dented · Oct 14, 2024 · N170FE · Boeing 7673S2F · Fuselage Floor Panel
  > MISSING 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 15/2024
- [SDR FDEA202404110455](https://openairdocs.org/sdr/FDEA202404110455.md): Warning Message · illuminated · Apr 11, 2024 · N170FE · Boeing 7673S2F · Hydraulic System, Main
  > AFTER 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 RESERVOI
- [SDR FDEA202206041376](https://openairdocs.org/sdr/FDEA202206041376.md): Former · cracked · Jun 4, 2022 · N170FE · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED 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 P1
- [SDR FDEA202012093079](https://openairdocs.org/sdr/FDEA202012093079.md): Former · cracked · Dec 9, 2020 · N170FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LT 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. TI
- [SDR FDEA202012083074](https://openairdocs.org/sdr/FDEA202012083074.md): Former · cracked · Dec 8, 2020 · N170FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LT 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-5720
- [SDR FDEA202012083073](https://openairdocs.org/sdr/FDEA202012083073.md): Former · cracked · Dec 8, 2020 · N170FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LT 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. INST
- [SDR FDEA202012083069](https://openairdocs.org/sdr/FDEA202012083069.md): Skin · delaminated · Dec 8, 2020 · N170FE · Boeing 7673S2F · Trailing Edge Flaps
  > RIGHT 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 REP
- [SDR FDEA202012033020](https://openairdocs.org/sdr/FDEA202012033020.md): Bracket · cracked · Dec 3, 2020 · N170FE · Boeing 7673S2F · Wing, Attach Fittings
  > LT 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 FDEA202012013025](https://openairdocs.org/sdr/FDEA202012013025.md): Attach Angle · cracked · Dec 1, 2020 · N170FE · Boeing 7673S2F · Nacelle/Pylon, Attach Fittings
  > NR 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 FDEA202011293053](https://openairdocs.org/sdr/FDEA202011293053.md): Frame · cracked · Nov 29, 2020 · N170FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON CENTER FITTING AT STA 329 INBOARD SIDE CRACKED. ACCOMPLISHED FRAME CRACK REPAIR AT NAC 329, IAW B767 SRM 54-52-71-2R.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N170FE/reports

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