# Service difficulty reports: N779FD A list on [N779FD](https://openairdocs.org/aircraft/N779FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA201810293047](https://openairdocs.org/sdr/FDEA201810293047.md): Battery · discharged · Oct 29, 2018 · N779FD · Boeing 757222 · Emergency Lighting > L1 DOOR EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT. REMOVED AND REPLACED LT EMERGENCY BATTERY PER AMM 33-51-07-2. OP'S CHECK GOOD. BATTERY ASSY P/N ON 2031-1A S/N 79304. - [SDR FDEA2018081491992](https://openairdocs.org/sdr/FDEA2018081491992.md): Girt Bar · lack of lube · Aug 9, 2018 · N779FD · Boeing 757222 · Emergency Equipment > LEFT ENTRY DOOR SLIDE LIGHT WILL NOT ILLUMINATE. CHECKED, CLEANED, AND LUBRICATED THE GIRT BAR AND SLIDERS. OPS NORMAL IAW MM 25-66-10-2, AND FIM 25-66-00 FT 802. - [SDR FDEA201709252718](https://openairdocs.org/sdr/FDEA201709252718.md): Skin · dented · Sep 25, 2017 · N779FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin > HORIZONTAL STABILIZER LEFT SIDE UPPER SKIN HAS DENT WITH POSSIBLE PUNCTURE LOCATED APPROX 16" FROM INBOARD EDGE AND 36" FROM LEADING EDGE. REMOVED DAMAGE AREA OF HORIZONTAL STAB LEFT UPPER SKIN, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR ALL IAW SRM 55-10 - [SDR FDEA201704281294](https://openairdocs.org/sdr/FDEA201704281294.md): Collar · cracked · Apr 28, 2017 · N779FD · Boeing 757222 · Passenger/Crew Doors > L1 DOOR HOLD-OPEN LOCK COLLAR CRACKED. R&R COLLAR OPS NORMAL PER MM 52-11-08-8-0. - [SDR FDEA201611244235](https://openairdocs.org/sdr/FDEA201611244235.md): Bottle · low pressure · Nov 24, 2016 · N779FD · Boeing 757222 · Escape Slide > DURING A PREFLIGHT INSPECTION, FOUND LEFT ENTRY DOOR SLIDE PRESSURE NOT IN GREEN RANGE. IAW AMM 25-66-01-6. - [SDR FDEA201607142447](https://openairdocs.org/sdr/FDEA201607142447.md): Connector · damaged · Jul 14, 2016 · N779FD · Boeing 757200 · Air Conditioning System Wiring > AT CRUISE ALT OF 35,000 FT LOST TEMPERATURE CONTROL OF COCKPIT SHORTLY AFTER WE EXPERIENCED A LOSS OF PRESURIZATION. CAB ALT WARNING LIGHT ILLUMINATED. EMERGENCY DESCENT INITIATED. AT 10,000 PRESSURIZATION RETURNED AND IT WAS ABLE TO CONTROL CABIN TO 4K. R - [SDR FDEA201607142448](https://openairdocs.org/sdr/FDEA201607142448.md): Motor · failed · Jul 14, 2016 · N779FD · Boeing 757222 · Cabin Pressure Control System > AT CRUISE ALT OF 35,000 FEET LOST TEMPERATURE CONTROL OF COCKPIT SHORTLY AFTER WE EXPERIENCED A LOSS OF PRESURIZATION. CABIN ALTITUDE WARNING LIGHT ILLUMINATED. EMERGENCY DESCENT INITIATED AT 10,000 FT. PRESSURIZATION RETURNED AND IT WAS ABLE TO CONTROL CABIN - [SDR FDEA201509012733](https://openairdocs.org/sdr/FDEA201509012733.md): Skin · dented · Sep 1, 2015 · N779FD · Boeing 757222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN STATION 1620 - 1640, STRINGER 23L - 24, HAS TWO EACH DENTS. ACCOMPLISHED EA F-5330-T0319198A FUSELAGE, PLATES & SKINS, SECTION 44 DENTS AT LT STATION 1620.00, STRINGER 23L. THIS IS A CAT B REPAIR, MAJOR. - [SDR FDEA201508112532](https://openairdocs.org/sdr/FDEA201508112532.md): Skin · dented · Aug 11, 2015 · N779FD · Boeing 757222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN BS 1600 - 1620, STRINGERS 21 - 22L, HAS ONE DENT & ONE OUTWARD DENT. REPAIRED IAW EA F-5330-T0319168 PT 1. THIS IS A CLASS B REPAIR, MAJOR IAW FORM 8100-9 DATED 08 05 2015. - [SDR FDEA201507232347](https://openairdocs.org/sdr/FDEA201507232347.md): Skin · dented · Jul 23, 2015 · N779FD · Boeing 757222 · Fuselage Main, Plate/Skin > INCOMING DENT ON FUSELAGE SKIN, BS 1703, 4 " BELOW STRINGER 17R. ACCOMPLISHED EA NR F-5330-T0319018 PT 1. FUSELAGE SKIN REPAIR ACCOMPLISHED ON EA 757-5361-16-F4986 & NR 00004521860001. MAJOR REPAIR CAT B. - [SDR FDEA201507182260](https://openairdocs.org/sdr/FDEA201507182260.md): Frame · corroded · Jul 18, 2015 · N779FD · Boeing 757222 · Fuselage Main, Frame > AFT PIT STATION 1480, FRAME HAS CORROSION, STRINGER 26R. R & R FRAME IAW SRM-51-40-02. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201507092181](https://openairdocs.org/sdr/FDEA201507092181.md): Frame Splice · corroded · Jul 9, 2015 · N779FD · Boeing 757222 · Fuselage Main, Frame > AFT PIT FRAME SPLICE, STATION 1500 LT HAS CORROSION. REMOVED CORROSION IAW SRM-51-10-02, OUT OF LIMITS IAW SRM-53-00-07 1A DETAIL II. ORIGINAL MAT.071", REMAINING MAT.053". R & R FRAME SPLICE AT STATION 1500 LT IAW-SRM-51-40-02. CAT A MAJOR REPAIR. - [SDR FDEA201507022136](https://openairdocs.org/sdr/FDEA201507022136.md): Door Frame · damaged · Jul 2, 2015 · N779FD · Boeing 757222 · Fuselage Main, Structure > MAIN DECK, LT FWD STUB FRAME AT BS 338 IS DAMAGED JUST BELOW DOOR INTERCOSTAL NR 3. IT WAS FOUND PORTION OF FRAME INBD FLANGE, BROKEN OFF AT NR 3 DOOR STOP FITTING AREA. NO ALLOWABLE LIMITS OR REPAIR ARE ESTABLISHED ON SRM. R & R FRAME SECTION IAW SRM 51-40 - [SDR FDEA201506191894](https://openairdocs.org/sdr/FDEA201506191894.md): Frame · dented · Jun 19, 2015 · N779FD · Boeing 757222 · Fuselage Main, Frame > AFT PIT FRAME STATION 1640, STRINGER 24L - 24R, REQUIRES REMOVAL TO FOM NR N00743. R & R FRAME IAW SRM-51-40-02. FABRICATED ON T15 1143093, EVALUATED FRAME, FOUND FRAME DENTED & WAS OUT OF LIMITS, NO ALLOWABLE DAMAGE IAW SRM. CAT A MAJOR REPAIR. - [SDR FDEA201506191886](https://openairdocs.org/sdr/FDEA201506191886.md): Floorbeam · corroded · Jun 19, 2015 · N779FD · Boeing 757222 · Fuselage Main, Floor Beam > DURING AFT DECK PLATE REPLACEMENT, FOUND FLOORBEAM AT STATION 1681, RBL 45 - RBL 48, CORRODED ON UPPER FLANGE. R & R STATION 1681 FLOORBEAM FROM MAT TYPE PN BAC 518-827A, BATCH 2699793 IAW DWG 146N5091 & SRM 51-10-02, 53-00-51-01, 51-40-02, 51-20-01 & MM 51 - [SDR FDEA201506171841](https://openairdocs.org/sdr/FDEA201506171841.md): Skin · dented · Jun 17, 2015 · N779FD · Boeing 757222 · Service Doors > LOWER FUSELAGE ACCESS DOOR 113AL INTERNAL SKIN DENTED & DEFORMED, PANEL RACK. R & R INNER SKIN, PN 141N6960-55, T15 1143784, IAW SRM 51-40-02 & DWG 141N6960. MAJOR REPAIR. - [SDR FDEA201506091736](https://openairdocs.org/sdr/FDEA201506091736.md): Frame · dented · Jun 9, 2015 · N779FD · Boeing 757222 · Fuselage Main, Frame > AFT CARGO BAY FRAME BS 1440, S26L - S27L HAS CORROSION. REMOVED CORROSION FROM THE FRAME IAW SRM 51-10-02. AFTER REMOVAL OF CORROSION, A DENT WAS NOTED ON UPPER FLANGE. FOUND OUT OF LIMITS IAW SRM SRM 53-00-07, FIG. 101, SHEET 1. REMOVED AND REPLACED THE F ## 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 = 'N779FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N779FD/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.