# Service difficulty reports: N101FE, cancelled Jan 23, 2003 A list on [N101FE, cancelled Jan 23, 2003](https://openairdocs.org/deregistered/N101FE-2003-01-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 01FDEA00973](https://openairdocs.org/sdr/01FDEA00973.md): Linkage · defective · Nov 9, 2001 · N101FE · Boeing 72722C · Landing Gear Retraction/Extension System > LANDING GEAR FAILED TO RETRACT AFTER T/O. REMOVED AND REPLACED LANDING GEAR VALVE ACTUATING LINK PER AMM 32-31-00-5. TEST OK FOR SERVICE. - [SDR 00FDEA00378](https://openairdocs.org/sdr/00FDEA00378.md): Spar · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Trailing Edge Flaps > DURING ROUTINE INSPECTION, RIGHT I/B MIDFLAP REAR SPAR UPPER CHORD FOUND CRACKED AT WING BUTT LINE 120 UPPER ROW FWD FASTENER HOLE. REMOVED AND REPLACED PER IAW MM 27-51-1. RIG AND OP CHECK FLAP PER IAW MM 27-51-0. - [SDR 00FDEA00377](https://openairdocs.org/sdr/00FDEA00377.md): Floorbeam · corroded · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor Beam > DURING ROUTINE INSPECTION, FLOORBEAM BS 640 FOUND CORRODED BEYOND LIMITS 4 INCHES LEFT OF NR 4 SEAT TRACK. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-8. - [SDR 00FDEA00376](https://openairdocs.org/sdr/00FDEA00376.md): Floorbeam · corroded · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor Beam > DURING ROUTINE INSPECTION, FLOORBEAM BS 344 FOUND CORRODED BEYOND LIMITS ON UPPER CHORD AT RBL 50. CUT OUT DAMAGE, FAB AND INSTALL PER IAW SRM 53-10-8. - [SDR 00FDEA00375](https://openairdocs.org/sdr/00FDEA00375.md): Floorbeam · corroded · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor Beam > DURING ROUTINE INSPECTION, FLOORBEAM BS 344, RT O/B END FOUND CORRODED BEYOND LIMITS ON LWR FLANGE. CUT OUT DAMAGE. FAB AND INSTALLED PER IAW SRM 53-10-8. - [SDR 00FDEA00374](https://openairdocs.org/sdr/00FDEA00374.md): Stringer · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Longeron/Stringer > DURING ROUTINE INSPECTION, STR 25R FOUND CRACKED BS 520. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-3. - [SDR 00FDEA00373](https://openairdocs.org/sdr/00FDEA00373.md): Floorbeam · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor Beam > DURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND SUPPORT DOUBLER IAW 51-40-3 & 51-30-2. - [SDR 00FDEA00372](https://openairdocs.org/sdr/00FDEA00372.md): Seat Track · corroded · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE INSPECTION, BS 870 FLOORBEAM FOUND CORRODED AT THE NR 1 SEAT TRACK. REMOVED AND REPLACED PER IAW SRM 51-10-6. FOUND WITHIN LIMITS IAW SRM 53-10-1, 51-30-2. - [SDR 00FDEA00371](https://openairdocs.org/sdr/00FDEA00371.md): Skin · corroded · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Plate/Skin > DURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3. FAB REPAIR PARTS PER IAW SRM 53-30-3. - [SDR 00FDEA00370](https://openairdocs.org/sdr/00FDEA00370.md): Support Bracket · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Spoilers > DURING ROUTINE INSPECTION, SUPPORT BRACKET FOR NR 7 SPOILER ACTUATOR FOUND CRACKED AT BOTH SIDES. REMOVED AND REPLACED NR 7 SPOILER AND ACTUATOR FITTING PER IAW SRM 51-10-1, 51-30-2, 27-62-001-4, AND 27-62-00. OPS CHECK GOOD. - [SDR 00FDEA00369](https://openairdocs.org/sdr/00FDEA00369.md): Beltframe · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Structure > DURING ROUTINE INSP BS 930 BELTFRAME FOUND CRACKED ON FWD SIDE OF STR 14R. REPAIRED BELTFRAME PER IAW FEDEX EO 7-2310-7-4330. - [SDR 00FDEA00368](https://openairdocs.org/sdr/00FDEA00368.md): Skin · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Plate/Skin > DURING ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. FUSELAGE SKIN REPAIR PER FEDEX EO 7-5330-7-2345 PART 2. - [SDR 00FDEA00367](https://openairdocs.org/sdr/00FDEA00367.md): Firewall · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Nacelle/Pylon, Bulkhead/Firewall > DURING ROUTINE INSP NR 2 ENG FIREWALL FOUND CRACKED AT APPROX 8 O''CLOCK POS AT FIRELOOP BRACKET. STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-10-1. - [SDR 00FDEA00366](https://openairdocs.org/sdr/00FDEA00366.md): Skin · cracked · Jun 5, 2000 · N101FE · Boeing 72722C · Cargo/Baggage Doors > DURING ROUTINE INSP, FWD LWR CARGO DOOR, EXT SKIN CRACKED IN LWR AFT CORNER. BLENDED OUT CRACK AND INSTALLED EXT DOUBLER IAW SRM 52-00-3. - [SDR 00FDEA00006](https://openairdocs.org/sdr/00FDEA00006.md): Connector · inoperative · Jan 5, 2000 · N101FE · Boeing 72722C · Landing Gear Position and Warning > 00-6 - REPEAT FROM 1/4/00; AFT T/O DOORS LIGHT AND L MAIN GEAR DOOR LIGHT REMAINED ON WITH GEAR HANDLE UP AND OFF. RECYCLED DID NOT CORRECT. ALL IND NORM WITH GEAR DOWN. REMOVED AND REPLACED CANNON PLUG ASSY IAW SWP 20-60-06. OPS CK DOOR FOUND NORM MEL CLE - [SDR 96FDEA01554](https://openairdocs.org/sdr/96FDEA01554.md): Nose Gear · malfunction · Sep 30, 1996 · N101FE · Boeing 72722 · Landing Gear Retraction/Extension System > WHEN LANDING GEARS WERE EXTENDED ON APPROACH, THE MAINS EXTENDED GREEN, BUT THE NOSE GEAR LIGHT REMAINED AMBER. NO NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL. CYCLED GEAR AND ALL GEAR EXTENDED NORMALLY. PERFORMED NOSE GEAR EXTENSION AND RETRACTION TEST ## 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 = 'N101FE' AND deregistration_id = 'N101FE-2003-01-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N101FE-2003-01-23/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.