# Service difficulty reports: N942DN, cancelled Nov 29, 2022 A list on [N942DN, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N942DN-2022-11-29.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DALA2019010200010](https://openairdocs.org/sdr/DALA2019010200010.md): Fastener · missing · Dec 31, 2018 · N942DN · Doug MD9030 · Wing, Plate/Skin > ON WALK AROUND FOUND RT WING APPROX 4 FEET FROM WING TIP FASTENER MISSING AND SEVERAL LOOSE. REMOVED RT WING O/B T/E FIXED WEDGE AND WING TIP PER AMM 57-20 FOR MTC ACCESS. COMPLIED WITH PRI 574177-14 REV 3. REINSTALLED RT WING O/B T/E FIXED WEDGE AND WING TIP - [SDR DALA2018102206189](https://openairdocs.org/sdr/DALA2018102206189.md): Beam · corroded · Oct 19, 2018 · N942DN · Doug MD9030 · Fuselage Main, Structure > CORROSION ON LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN CTR CARGO COMPARTMENT. CORROSION LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN CTR CARGO COMPARTMENT (UT) WAS ACOMPLISHED PER SPM NDT 04-00-07 PAR. 5 FIG 3SHEET 1 AND 2 NOMINA - [SDR DALA2018102206188](https://openairdocs.org/sdr/DALA2018102206188.md): Beam · corroded · Oct 19, 2018 · N942DN · Doug MD9030 · Fuselage Main, Structure > CORROSION ON LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN AFT CARGO COMPARTMENT. CORROSION LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN AFT CARGO COMPARTMENT (UT) WAS ACOMPLISHED PER SPM NDT 04-00-07 PAR. 5 FIG 3SHEET 1 AND 2 NOMINA - [SDR DALA2018082875305](https://openairdocs.org/sdr/DALA2018082875305.md): Window · failed · Aug 26, 2018 · N942DN · Doug MD9030 · Passenger Compartment Windows > WINDOW AT 16A CRACKED IN FLIGHT, APPEARS TO BE OUTER PANE THAT DELAMINATED. OUTER PART OF WINDOW SEPARATED FROM AIRCRAFT IN FLIGHT. PERFORMED INSPECTION ON LT ENGINE WITH NO DEFECTS IAW AMM 05-51-19. REMOVED AND REPLACED PASSENGER COMPARTMENT WINDOW ASSY IAW - [SDR DALA2018032601925](https://openairdocs.org/sdr/DALA2018032601925.md): Cable · damaged · Mar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic Fairings > AFT ENTRY DOOR EMERGENCY TAILCONE RELEASE FAILED. DOOR ROD FAILED TO RELEASE CABLE QUADRANT AT DOOR UPPER FRAME. PULL TEST EXCEEDED LIMIT OF 15LBS. ACTUAL PULL TEST 40LBS TO BY PASS DOOR IN. LUBED CABLE ND REPLACED CABLE IAW AMM 20-52. OPS NORMAL WITHIN LIMIT - [SDR DALA2018032601924](https://openairdocs.org/sdr/DALA2018032601924.md): Cable · frayed · Mar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic Fairings > TAILCONE EMERGENCY RELEASE LOCK CABLE FOR SUPPORT FITTING FRAYED AT CABLE BALL END. REPLACED THE CABLE IAW AMM 20-52. - [SDR DALA2018032601923](https://openairdocs.org/sdr/DALA2018032601923.md): Cable · damaged · Mar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic Fairings > TAILCONE EMERGENCY RELEASE LOCK CABLE FORWARD OF TEE PIN FAILED TO RELEASE FROM SUPPORT FITTING, WHEN THE TEE PIN CAME OUT. REPLACED THE CABLE IAW AMM 20-52. - [SDR DALA2017102907894](https://openairdocs.org/sdr/DALA2017102907894.md): Line · leaking · Oct 28, 2017 · N942DN · Doug MD9030 · Potable Water System > EXPERIENCED SMOKE AND FUMES IN THE AC CABIN AFTER PUSHBACK. FLIGHT CREW HAD TUG DRIVER RETURN AC TO JETWAY AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND A CRACKED WATER LINE ABOVE THE WATER HEATER LOCATED IN THE F/CLASS LAV. THE WATER LINE WAS DRIPPING - [SDR DALA2016102007433](https://openairdocs.org/sdr/DALA2016102007433.md): Unknown · odor · Oct 18, 2016 · N942DN · Doug MD9030 · Air Distribution System > DURING TAKEOFF AND LANDING, CREW REPORTED A STRONG ODOR OF BURNING RUBBER IN COCKPIT AND FORWARD CABIN. ODOR DISSIPATES RAPIDLY. TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. - [SDR DALA2016100407076](https://openairdocs.org/sdr/DALA2016100407076.md): Frame · cracked · Sep 29, 2016 · N942DN · Doug MD9030 · Fuselage Main, Frame > NOSE LANDING GEAR CUTOUT LEFT FRAME CRACKED AT GUIDE FORWARD UPPER FASTENER ATTACH HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-90-01. - [SDR DALA2016100407077](https://openairdocs.org/sdr/DALA2016100407077.md): Web · cracked · Sep 26, 2016 · N942DN · Doug MD9030 · Fuselage Miscellaneous Structure > FORWARD WET AREA UNDER G7 GALLEY, WEB CRACKED BOTTOM SIDE AT FASTENER. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-20-02. - [SDR DALA2016051904130](https://openairdocs.org/sdr/DALA2016051904130.md): Valve · cracked · May 16, 2016 · N942DN · Doug MD9030 · Hydraulic Indicating System > IN FLIGHT, HYDRAULIC QTY DROPPED TO 4. CREW RAN QRH PROCEDURE AND SHUT OWN RT HYDRAULIC SYSTEM. DURING DESCENT, IAW THE QRH, ATTEMPTED TO RE-PRESSURIZED THE RT SYSTEM. THE RT SYS INDICATED 3000 PSI BUT QTY DROPPED TO 0. MAINTENANCE FOUND THE LT WING OTBD A - [SDR DALA2016042103159](https://openairdocs.org/sdr/DALA2016042103159.md): Structure · damaged · Apr 18, 2016 · N942DN · Doug MD9030 · Passenger/Crew Doors > L1 DOOR DAMAGED. REPAIRED EDGE FLANGE IAW SRM 52-01-01. - [SDR DALA2014102905825](https://openairdocs.org/sdr/DALA2014102905825.md): Structure · cracked · Oct 29, 2014 · N942DN · Doug MD9030 · Horizontal Stabilizer Structure > FOUND CRACK INDICATION ON FIRST FASTENER HOLE ABOVE ZFS=52.267-M. REAMED HOLE TO FINAL SIZE OF.231" IAW DWG SG09550005. INSTALLED BUSHING, FABRICATED STRAP AND INSTALLED REPAIR STRAP IAW DWG SG09550005-7003. - [SDR DALA2014102905824](https://openairdocs.org/sdr/DALA2014102905824.md): Skate Angle · cracked · Oct 28, 2014 · N942DN · Doug MD9030 · Vertical Stabilizer > FORWARD RT INNER VERTICAL STABILIZER ATTACH ANGLE HAS A FOUR INCH CRACK. R & R INNER SKATE ANGLE IAW DWG 5912188. - [SDR DALA2014102905826](https://openairdocs.org/sdr/DALA2014102905826.md): Skin · cracked · Oct 27, 2014 · N942DN · Doug MD9030 · Fuselage Main, Plate/Skin > SKIN CRACKED AT BS 1475, LONGERON 2R. UNDER INTERNAL SKATE ANGLE. REPAIRED SKIN CRACK IAW DWG SG 90530003. - [SDR DALA13072079242](https://openairdocs.org/sdr/DALA13072079242.md): Structure · damaged · Dec 25, 2013 · N942DN · Doug MD9030 · Cargo/Baggage Doors > LIGHTNING STRIKE ON FASTENER AFT CORNER OF MID CARGO DOOR. REPAIRED IAW ERA 521840-14, SECTION I, REV O. REF LP 1243580, DTA. - [SDR DALA13003809242](https://openairdocs.org/sdr/DALA13003809242.md): Skin · corroded · Jan 18, 2013 · N942DN · Doug MD9030 · Fuselage Main, Plate/Skin > CORROSION FOUND BS 1172 RT AFT FUSELAGE TWO INCHES ABOVE RBL 28, BETWEEN LONGERON 27-28. REMOVED CORROSION CUT-OUT DAMAGE AREA FABRICATED, LOCATED, TREATED, PRIMED AND INSTALLED REPAIRED PARTS IAW SRM 53-30-01, FIG 9 AND SRM 51-10-03, FIG 3 AT STA 1172 RT AFT - [SDR DALA13004329242](https://openairdocs.org/sdr/DALA13004329242.md): Skin · corroded · Jan 16, 2013 · N942DN · Doug MD9030 · Fuselage Main, Plate/Skin > DURING HMV, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1145.5 AND L29R. DAMAGE WAS REPAIRED IAW ER/A 504831-14, SECTION I. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER REPAIR AND TAPERED SHIM. TREATED, PRIMED AND INSTALLED REPAIR P - [SDR DALA13003079242](https://openairdocs.org/sdr/DALA13003079242.md): Spar Cap · corroded · Jan 15, 2013 · N942DN · Doug MD9030 · Wing Spar > WHILE IN SERVICE, CORROSION WAS FOUND ON THE RT WING FRONT SPAR LOWER CAP HORIZONTAL FLANGE AT XRS=531.700. THE REPAIR WAS ACCOMPLISHED IAW ER/A 510556-14, SECTION I. - [SDR DALA13003069242](https://openairdocs.org/sdr/DALA13003069242.md): Longeron · cracked · Jan 11, 2013 · N942DN · Doug MD9030 · Fuselage Main, Longeron/Stringer > WHILE IN SERVICE, A CRACK WAS FOUND ON FUSELAGE LONGERON 2R BETWEEN BS 1458-1475. ACCOMPLISHED A SPLICE REPAIR AND INSTALLED A 0.160" THICK STRAP. INSTALLED REPAIR IAW PROCESS STANDARD 900-5-1 NR 04. COMPLIED WITH ER/A 510485-14, REV "O". - [SDR DALA13003049242](https://openairdocs.org/sdr/DALA13003049242.md): Skin · corroded · Jan 11, 2013 · N942DN · Doug MD9030 · Wing, Plate/Skin > WHILE IN SERVICE, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE LT LOWER WING SKIN PANEL OTBD OF XRS=545.380 AT THE T/E. REPAIR WAS ACCOMPLISHED IAW ER/A 510483-14 SECTION I. - [SDR DALA13001999242](https://openairdocs.org/sdr/DALA13001999242.md): Spar Cap · corroded · Jan 10, 2013 · N942DN · Doug MD9030 · Horizontal Stabilizer, Spar/Rib > CORROSION REPAIR ON RT HORIZONTAL STABILIZER UPPER FRONT SPAR CAP AND LT HORIZONTAL STABILIZER LOWER FRONT SPAR CAP BARREL NUT FORWARD AND AFT HOLES IAW ER/A 510432-14, ACCOMPLISH SECTION I AT THE PRIOR TO SERVICE VISIT. ASSOCIATED ER/A 14-510432 ADDED FOR AC - [SDR DALA12017409242](https://openairdocs.org/sdr/DALA12017409242.md): Seat Track · gouged · Dec 29, 2012 · N942DN · Doug MD9030 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK, RBL 22, BS 436 GOUGED. CUT OUT DAMAGED AREA. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-40-01, FIG 6, VOL I. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-40-01, FIG 6, VOL I. - [SDR DALA12017249242](https://openairdocs.org/sdr/DALA12017249242.md): Door Frame · cracked · Dec 22, 2012 · N942DN · Doug MD9030 · Fuselage Main, Structure > DURING SERVICE CHECK, MX FOUND L1 DOOR AFT INTERNAL UPPER DOOR FRAME CRACKED. REMOVED OLD BEAM. FABRICATED AND INSTALLED NEW BEAM IAQ SRM 51-30-01. ## 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 = 'N942DN' AND deregistration_id = 'N942DN-2022-11-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N942DN-2022-11-29/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.