# Service difficulty reports: N78285

A list on [N78285](https://openairdocs.org/aircraft/N78285.md).

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

Page 1 of 2 · 63 reports

- [SDR CALA2026042815747](https://openairdocs.org/sdr/CALA2026042815747.md): Support Frame · gouged · Apr 23, 2026 · N78285 · Boeing 737824 · Aerodynamic Fairings
  > LEFT-SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA727 JUST ABOVE FLAP TRACK #4 HAS A DEEP GOUGE. REPAIRED SUPPORT FRAME LOCATED AT L/H WING TO BODY FAIRING STA 727 AS PER AAR WORK INSTRUCTIONS ESR 33-15106 AND EC/RA 5360-02134.
- [SDR CALA2026042715727](https://openairdocs.org/sdr/CALA2026042715727.md): Stiffener · cracked · Apr 23, 2026 · N78285 · Boeing 737824 · Horizontal Stabilizer Miscellaneous Structure
  > EA5510-01843 REV. J. CRACK. LEFT HORIZONTAL STAB STA 92,7 INBOARD SIDE OF RIB #1 HAD EVIDENCE OF CRACK AT VERTICAL STIFFINER #2 TRANSITION RADIO. REF AAR NR 100015416. REPAIRED STIFFENER NO. 2 AT L/H HORIZONTAL STAB STA 92.7 RIB #1 AS PER SRM 55-10-09-2R-5.
- [SDR CALA2026042815746](https://openairdocs.org/sdr/CALA2026042815746.md): Frame · gouged · Apr 22, 2026 · N78285 · Boeing 737824 · Fuselage Main, Frame
  > APU DOOR ASSY FRAME HAS A DEEP GOUGE LOCATED AFT OF THE AFT HINGE. REPAIRED APU DOOR ASSY FRAME STA 1154.60 LBL 18 AS PER EC/RA 5240-01751.
- [SDR CALA2026042415676](https://openairdocs.org/sdr/CALA2026042415676.md): Hinge · cracked · Apr 22, 2026 · N78285 · Boeing 737824 · Fuselage, Door Hinge
  > CRACKED APU DOOR ASSY INTERNAL @ APPROXIMATELY STA 1020 HINGE AREA FWD AND AFT SIDE. FABRICATED 2EA HINGE FRAME AT APU DOOR ASSY INTERNAL STA 1020 FWD AND AFT IAW DWG 148A6353-127 AND DWG 148A6353-128. INSTALLED IAW SRM 51-40-02-0G-0.
- [SDR CALA2026050516020](https://openairdocs.org/sdr/CALA2026050516020.md): Skin · cracked · Apr 20, 2026 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR, I/B ROW. CRACK LENGTH - 3/4". REPAIRED LEFT HORIZONTAL STAB LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR IAW SRM 55-10-01-2R-11.
- [SDR CALA2026041715428](https://openairdocs.org/sdr/CALA2026041715428.md): Skin · cracked · Apr 14, 2026 · N78285 · Boeing 737824 · Leading Edge Devices
  > LEFT WING SLAT # 3. ACTUATOR ATTACHED POINT CRACKED/FASTENERS PULL IN INS-206. REPAIRED SLAT NO.3 NOSE SKIN LOWER SURFACE AT THE ACTUATOR ATTACH POINTS AREA AS PER SRM 57-42-01-2R-8 ALTERNATIVE 1
- [SDR CALA2026041615405](https://openairdocs.org/sdr/CALA2026041615405.md): Angle · cracked · Apr 14, 2026 · N78285 · Boeing 737824 · Leading Edge Devices
  > SLAT NR 3 COVE ANGLE CRACKED. REMOVED AND REPLACED SLAT NR 3 COVE ANGLE IAW SRM 51-40-02-0G-0, AND DRAWING 114A5030 SHEET 6 AND SHEET 7.
- [SDR CALA2026042915818](https://openairdocs.org/sdr/CALA2026042915818.md): Hinge Fitting · cracked · Apr 10, 2026 · N78285 · Boeing 737824 · Fuselage, Door Hinge
  > CRACK FOUND AT R-1 DOOR CUTOUT FWD SIDE SEAL DEPPRESOR. REF AAR NR 100015583. REMOVED AND REPLACED R1 DOOR CUTOUT HINGE FITTING P/N 141A8358-4 AS PER SRM 51-40-02-0G-0 AND DRAWINGS 141A8350 SHEETS 14 AND 15.WORK ACCOMPLISHED BY V929396. FOR INFO ENTRY REMOVED
- [SDR CALA2026041515372](https://openairdocs.org/sdr/CALA2026041515372.md): Web · dented · Apr 10, 2026 · N78285 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND LARGE DENT FLIGHT COMPARTMENT FLOOR LBL 15 STA 259. REPAIRED FLIGHT COMPARTMENT FLOOR STRUCTURE WEB APPROX STA 259 LBL 15 AS PER SRM 53-10-51-2R-2.
- [SDR CALA2026041315280](https://openairdocs.org/sdr/CALA2026041315280.md): Stub Frame · cracked · Apr 10, 2026 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > R1 DOOR OF THE FWD GALLEY DOOR STUB FRAME BS 294.5 CRACKED BETWEEN STR7R & STR9R (LENGTH.750). REMOVED AND REPLACED THE R1 DOOR STUB FRAME IAW SRM 51-40-02-0G-0, DWG 141A8370, SHEET 9, AND DWG 141A8380, SHEET 13, 14, & 17.
- [SDR CALA2026040215046](https://openairdocs.org/sdr/CALA2026040215046.md): Seat Track · gouged · Mar 31, 2026 · N78285 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGE FOUND AT PASSENGER CABIN SEAT TRACK STA 520 LBL45. AAR N/R 100015511. REPAIRED SEAT TRACK AT PASSENGER CABIN STA 520 LBL 45 AS PER SRM 53-00-52-2R-4. WORK ACCOMPLISHED BY V929396. LOG PAGE 8398960 NONROUTINE 100015511
- [SDR CALA2026040215044](https://openairdocs.org/sdr/CALA2026040215044.md): Seat Track · corroded · Mar 31, 2026 · N78285 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND AT PASSENGER CABIN SEAT TRACK STA 380 RBL24. REF AAR N/R 100015510. REMOVED AND REPLACED SEAT TRACK P/N 143A5310U35 AT PASSENGER CABIN STA 380 RBL 24 AS PER SRM 51-40-02-0G-0 AND DRAWING 143A5300 SHEET 54.
- [SDR CALA2026040114991](https://openairdocs.org/sdr/CALA2026040114991.md): Floorbeam · corroded · Mar 24, 2026 · N78285 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA STA 986.5 FLOORBEAM HAS CORROSION AT FASTENER HOLE LBL 4.REF AAR NR 100015282. REPAIRED FLOORBEAM LOCATED AT STA 986.5 AT PASSENGER CABIN AFT WET AREA (LBL 4) AS PER SRM 53-00-51-2R-1.
- [SDR CALA2026033114961](https://openairdocs.org/sdr/CALA2026033114961.md): Floorbeam · corroded · Mar 24, 2026 · N78285 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA BS 986.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES AT RBL 23, RBL 30 AND RBL 43. REPAIRED FLOOR BEAM LOCATED AT BS 986.5 AT PASSENGER CABIN AFT WET AREA (RBL 23, RBL 30, RBL 43) AS PER EC/RA 5321-01429.
- [SDR CALA2026033114960](https://openairdocs.org/sdr/CALA2026033114960.md): Floorbeam · corroded · Mar 24, 2026 · N78285 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA BS 986.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES AT LBL 30 AND LBL 43. REPAIRED FLOOR BEAM LOCATED AT STA 986.5 AT PASSENGER CABIN AFT WET AREA (LBL 30 AND 43) AS PER EC/RA 5321-01429.
- [SDR CALA2026020213480](https://openairdocs.org/sdr/CALA2026020213480.md): Battery · no test · Jan 31, 2026 · N78285 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - AFT SECTION OF THE PASSENGER CABIN EMERGENCY SEAT LIGHTS ARE INOP REPLACED EMERGENCY POWER BATTERY PACK FOR AFT SEC OF EMERGENCY PROX LIGHTS ON SEATS WITH REF TO AMM TASK 33-51-06-960-80
- [SDR CALA2025091909043](https://openairdocs.org/sdr/CALA2025091909043.md): Attach Angle · cracked · Sep 17, 2025 · N78285 · Boeing 737824 · Fuselage Main, Attach Fittings
  > STATION 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY RBL 9.0. REPAIRED CRACKED UPPER ATTACH ANGLE AT STATION 663 VAPOR BARRIER AND RBL 9.0 IAW SRM 57-10-10-2R-5 REPAIR 5 AND ACCOMPLISHED FUEL, LEAK CHECK IAW AMM 28-11-00, LEAK CHECK GOOD
- [SDR CALA2025091909042](https://openairdocs.org/sdr/CALA2025091909042.md): Attach Angle · cracked · Sep 17, 2025 · N78285 · Boeing 737824 · Fuselage Main, Attach Fittings
  > LEFT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY LBL 9.0 SUPPORT TASK NSA EMX NR 00064 SFR REPORTING ONLY REPAIRED CRACKED UPPER ATTACH ANGLE AT STATION 663 AND LBL 9.0 IAW SRM 57-10-10-2R-5 REPAIR 5 AND ACCOMPLISHED FUEL LEAK CHECK IA
- [SDR CALA2025041703921](https://openairdocs.org/sdr/CALA2025041703921.md): Girt Bar · unpacked · Apr 15, 2025 · N78285 · Boeing 737824 · Emergency Equipment
  > SLIDE AT DOOR 1R MAY BE LOOSE FROM HOUSING FOUND DOOR 1R SLIDE GIRT MATERIAL SLIGHTLY PULLED OUT. GIRT TUCKED BACK IN AND RESECURED VELCRO. REF. AMM 25-66-01.
- [SDR CALA2025010900062](https://openairdocs.org/sdr/CALA2025010900062.md): Battery Pack · inoperative · Jan 6, 2025 · N78285 · Boeing 737824 · Emergency Lighting
  > EMERGENCY AISLE LIGHTS AT FIRST CLASS SEATS INOP. SUPPORT TASK N SA EMX N/R 00185. REMOVED AND REPLACED BATTERY PACK AT M1674 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-825.
- [SDR CALA2024090302371](https://openairdocs.org/sdr/CALA2024090302371.md): Sealant · damaged · Sep 1, 2024 · N78285 · Boeing 737824 · Flight Compartment Windows
  > PASSING 13000 LOUD WHOOSHING NOISE FROM R1. FOUND SPEED TAPE LIFTING AND SEALNT BLOWN OUT OF GROOVE. CLEANED AND REAPPLIED SEALANT IRW MM 56-11-11-400-801. NO OTHER DEFECTS NOTED. PRESSURIZED TO 4.5PSI WITH NO LEAKS ON WINDOW NOTED. CHANGED CORRCETION ATA TO
- [SDR CALA2024043001270](https://openairdocs.org/sdr/CALA2024043001270.md): Windshield · damaged · Apr 27, 2024 · N78285 · Boeing 737824 · Flight Compartment Windows
  > LOUD SQUEAL FROM FO WINDOW ABOVE 6.2 PSI DEBRIEFED FLIGHT CREW. FLIGHT CREW STATES NOISE WAS FROM LEADING EDGE OF FO SLIDING WINDOW, NOISE STARTED AT A DIFFERENTIAL PRESSURE 6.2PSI AND CONTINUED WITH NO OBVIOUS STOPPING POINT DURING DEPRESSURIZATION. FLIGHT CR
- [SDR CALA2024040500983](https://openairdocs.org/sdr/CALA2024040500983.md): Window Frame · cracked · Apr 4, 2024 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > (SUPPORT TASK) COCKPIT LH NO. 1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER CRACK REPAIRED PER EA 5310-04554 CARD IS FOR REPORTING ONLY NO M AIT ON THIS NR REPAIR WAS ACCOMPLISHED ON OP 4005. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 4066 NR 20611 BY M
- [SDR CALA2024040500982](https://openairdocs.org/sdr/CALA2024040500982.md): Window Frame · cracked · Apr 4, 2024 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > (SUPPORT TASK) COCKPIT RH NO. 1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER. CRACK REPAIRED PER EA 5310-04554 CARD IS FOR REPORTING ONLY NO M AIT ON THIS NR REPAIR WAS ACCOMPLISHED ON OP 4003. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 4066 NR 20612 BY
- [SDR CALA2023052601654](https://openairdocs.org/sdr/CALA2023052601654.md): Skin · damaged · May 24, 2023 · N78285 · Boeing 737824 · Vertical Stabilizer, Plate/Skin
  > R/H HORIZONTAL STAB LOWER INSPAR SKIN REQUIRES FABRICATION AND INSTALLATION OF DOUBLER TO INCORPORATE 3 EACH REMOVED SKIN DOUBLERS AND 4 EACH NEW SKIN CRACK CUT-OUTS BTWN APPROX STAB STATIONS 101.90 TO 138.5. CYCLES REF SRM 55-10-01-2R-11 REPAIR 11 PAR.5A. (SE
- [SDR CALA2020072701080](https://openairdocs.org/sdr/CALA2020072701080.md): Controller · inoperative · Jul 27, 2020 · N78285 · Boeing 737824 · Cabin Temperature Control System
  > RT PACK LIGHT CAME ON DURING CLIMB OUT RAN CHECKLIST STILL STAYE D ON LOCKING DO TO MX DIVERSION UNLOCKED FOR SIGN OFF PERFORMED RIGHT PACK/ZONE TEMP. CONTROL BITE REF. AMM 21-61-00, FOUND "AIR CONDITIONING PACK CONTROL RIGHT AC" C/B (P6-4/B11) OPEN; RESET C/B
- [SDR CALA2020052200993](https://openairdocs.org/sdr/CALA2020052200993.md): Skin · damaged · May 21, 2020 · N78285 · Boeing 737824 · Cargo/Baggage Doors
  > NUMEROUS DENTS AND CREASES ON FWD CARGO COMPARTMENT DOOR. REMOVED AND REPLACED CARGO DOOR SKIN AND REINSTALLED FWD CARGO D DOOR IAW AMM 52-31-10 AND SRM 52-30-11.
- [SDR CALA2020052200988](https://openairdocs.org/sdr/CALA2020052200988.md): Fitting · cracked · May 20, 2020 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > BS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 15.04 CRACKED. REMOVED AND REPLACED AT BS 540 SPAR ANGLE AT LBL 15.04 CRACKED.
- [SDR CALA2020052200987](https://openairdocs.org/sdr/CALA2020052200987.md): Fitting · cracked · May 20, 2020 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > BS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 6.01 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 6.01.
- [SDR CALA2020052200986](https://openairdocs.org/sdr/CALA2020052200986.md): Fitting · cracked · May 20, 2020 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > B737-53-3-0716 STA 540 WING CENTER SECTION UPPER FRONT SPAR AT RBL 15.04 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 15.04.
- [SDR CALA2020052200985](https://openairdocs.org/sdr/CALA2020052200985.md): Fitting · cracked · May 20, 2020 · N78285 · Boeing 737824 · Fuselage Main, Structure
  > BS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 6.01 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 6.01.
- [SDR CALA2020052200984](https://openairdocs.org/sdr/CALA2020052200984.md): Spar · cracked · May 20, 2020 · N78285 · Boeing 737824 · Wing Spar
  > BS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 32.53 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 32.53. REMOVED AND REPLACED AT BS 540 WING CENTER SECTION UPPER FRO SPAR ANGLE AT RBL 32.53.
- [SDR CALA2020052200973](https://openairdocs.org/sdr/CALA2020052200973.md): Battery Pack · no test · May 19, 2020 · N78285 · Boeing 737824 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHT ZONES FAIL FUNCTIONAL CHECKS.
- [SDR CALA2020050900940](https://openairdocs.org/sdr/CALA2020050900940.md): Rib · cracked · May 6, 2020 · N78285 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > EA 5510-01843 R/H HORRZANTAL STA RIB STA 92.70 HAS CRACK AT NO.2 VERTICAL STIFFENER TRANSATION RADIUS AND CRACKED VERTICAL WEB. REF BY PEMCO NR 2759N577. REPAIRED RH HORIZ STAB STIFFENER #2 IAW SRM 55-10-09RPR4 FIG202 AND REPAIRED LOWER SKIN IAW B737-800 SRM 5
- [SDR CALA2020050900939](https://openairdocs.org/sdr/CALA2020050900939.md): Skin · cracked · May 6, 2020 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > EA 5510-01843 REV H OP 001:RH HORZ STAB AFT OF FWD SPAR, STA 147.9, 30.5 TO 31.25". CRACK. REF BY PEMCO NR 2759N537 REPAIRED RH HORIZ STAB STIFFENER #2 IAW SRM 55-10-09RPR4 FIG202 AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01 RPR11 FIG204. INSP REQUIREMENT
- [SDR CALA2020050900935](https://openairdocs.org/sdr/CALA2020050900935.md): Skin · cracked · May 5, 2020 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > EA 5510-01843 REV H OP 001: LH HORZ STAB AFT OF FWD SPAR, STA 157.1, 22.5 TO 23", CRACK NOTED. REF TO PEMCO NR 2759N535. REMOVED.5" CRACK FROM THE LH HORZ STAB LOWER SKIN AT STA 157.1 IAW B737-800 SRM 55-10-01 REPAIR 11, FABBED AND INSTALL 21"X17" REPAIR IAW
- [SDR CALA2020050900934](https://openairdocs.org/sdr/CALA2020050900934.md): Skin · cracked · May 5, 2020 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > EA 5510-01843 REV H OP 001: LH HORZ STAB AFT OF FWD SPAR, STA 147.90, 8" TO 8.5", CRACK NOTED. REF TO PEMCO NR 2759N533. REMOVED.5" CRACK FROM THE LH HORZ STAB LOWER SKIN AT STA 147.9 IAW B737-800 SRM 55-10-01 REPAIR 11, FABBED AND INSTALL 9"X11" REPAIR IAW B
- [SDR CALA2020050900933](https://openairdocs.org/sdr/CALA2020050900933.md): Skin · cracked · May 5, 2020 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > EA 5510-01843 REV H OP 001: LH HORZ STAB AFT OF FWD SPAR, 1. STA 129.5, 32.5" TO 33.5", CRACK NOTED. REF TO PEMCO NR 2759N531 REMOVED 1" CRACK FROM THE LH HORZ STAB LOWER SKIN AT STA 129.5 IAW B737-800 SRM 55-10-01 REPAIR 11, FABBED AND INSTALL 9"X11" REPAIR I
- [SDR CALA2020041700844](https://openairdocs.org/sdr/CALA2020041700844.md): Pressure Web · cracked · Apr 15, 2020 · N78285 · Boeing 737824 · Fuselage Main, Bulkhead
  > B737-57-3-0634 RIGHT CENTER WING REAR SPAR VERTICAL PRESSURE WEB CRACKED BEHING SPOILER HYDROLIC CONTROL VALVE. REF BY PEMCO NR 2759N31. PERFORMED REPAIR ON RH CTR WING REAR SPAR VERT PRESSURE WEB AT STA 663.75 RBL 25.00 TO RBL 45.64 IAW SRM 57-10-10 REP 3 ALT
- [SDR CALA2019031100388](https://openairdocs.org/sdr/CALA2019031100388.md): Oven · odor · Mar 9, 2019 · N78285 · Boeing 737824 · Buffet/Galleys
  > ELECTRICAL BURN SMELL NOTICED BY FLIGHT ATTENDANTS AT AFT GALLY AREA WHILE USING OVEN 425. INSPECTED AND GALLEY AREA FOR ELECTRICAL SMELL AND FOUND OVEN AT POSITION 425 AT FAULT REMOVED AND REPLACED OVEN AND OPS CKS GOOD, ALSO RAN ALL OVENS AND COFFEE MAKER
- [SDR CALA2017102003701](https://openairdocs.org/sdr/CALA2017102003701.md): Lamp · inoperative · Oct 20, 2017 · N78285 · Boeing 737824 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOPERATIVE. EXTERIOR. REPLACED THE LAMPS IAW MM 33-51-00. OPS CHECKED GOOD.
- [SDR CALA2017100903564](https://openairdocs.org/sdr/CALA2017100903564.md): Lens · loose · Oct 9, 2017 · N78285 · Boeing 737824 · Emergency Lighting
  > R2 DOOR EMERGENCY EXIT SIGN LENS DETACHED. REPLACED THE LENS, OPS OK.
- [SDR CALA2017020300227](https://openairdocs.org/sdr/CALA2017020300227.md): Skin · cracked · Feb 2, 2017 · N78285 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER HAS A POSSIBLE CRACK AT L.E. HSS 133.15 APROX. 6 INCHES INBOARD OF EXISTING REPAIR. PERFORMED REPAIR IAW SRM 55-10-01.
- [SDR CALA2016100300712](https://openairdocs.org/sdr/CALA2016100300712.md): Door · dirty · Sep 30, 2016 · N78285 · Boeing 737824 · Landing Gear Retraction/Extension System
  > GEAR DID NOT COME UP AFTER TAKEOFF, ALL GREEN IN THE DOWN POSITION CLEANED MANUAL EXTENSION DOOR AND SWT REF MM32-34-00-100-801C1. ACP OPERATIONAL CHECKS REF MM32-32-00-710-801 AND 32-34-00-730- 801. LANDING GEAR EXT AND RETRACTION OPERATES NORMALLY.
- [SDR CALA2016072800466](https://openairdocs.org/sdr/CALA2016072800466.md): Flap System · malfunctioned · Jul 28, 2016 · N78285 · Boeing 737824 · Leading Edge Slat Control System
  > LE FLAP TRANSIT LIGHT ILLUIMATED AND FLAP NEEDLE SPLIT WHEN FLAPS SELECTED TO 5. EMERGENCY DECLARED. RAN FLAPS TRAILING EDGE FLAPS DISAGREE CHECKLIST.SPLIT WENT AWAY WHEN HANDLE WAS POSITIONED UP. RAN BITE CHECK ON FSEU, SHOWED NO EXISTING FAULTS. RAN FLA
- [SDR CALA2016020800094](https://openairdocs.org/sdr/CALA2016020800094.md): Unknown · malfunctioned · Feb 6, 2016 · N78285 · Boeing 737824 · Cabin Pressure Control System
  > AIR RETURN FOR CABIN ACT LIGHT & HORN ON IN CLIMB. ACFT WOULD NOT PRESS. PRESSURIZATION TESTED GOOD. PRESSURIZATION SYS GND BITE TEST IAW MM 21-31-00, CHECKED OK. SUSPECT PACKS WERE NOT TURNED ON.
- [SDR CALA2014081801130](https://openairdocs.org/sdr/CALA2014081801130.md): Frame · cracked · Aug 16, 2014 · N78285 · Boeing 737824 · Fuselage Main, Frame
  > AT STATION 706L BETWEEN STRINGER 8 & 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, THE FRAME HAS A CRACK INDICATION AT THE INBD ATTACHMENT RIVET. CORRECTED CUT OUT FRAME & REPAIR FRAME IAW RES NR 2007378-20 & SB 737-25-1
- [SDR CALA2014081801128](https://openairdocs.org/sdr/CALA2014081801128.md): Seat Track · damaged · Aug 15, 2014 · N78285 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK LBL 24.75 HAS INBD AFT FLANGE A HOLE WITHOUT MARKING AT STATION 727B. ACCOMPLISHED REPAIR AT CABIN SEAT TRACK FLOORBEAM IAW ECRA 53-20-02294. THIS ECRA PROVIDES APPROVED PERMANENT REPAIR INSTRUCTIONS FOR THE DAMAGED CHORD.
- [SDR CALA2014081501127](https://openairdocs.org/sdr/CALA2014081501127.md): Battery Pack · defective · Aug 15, 2014 · N78285 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK FAILED ON CUSTOMER CARD 58-3 300-1-7500. TROUBLE SHOT & FOUND BATTERY PACKS AT POSITIONS M1670 & M1676 DEFECTIVE IAW AMM 33-51-06 & SSM 33-51-21. R & R EMER BATTERY PACKS. OPERATIONS CHECK OF EMER LIGHT BATTERY PACKS NORMAL
- [SDR CALA2014081501126](https://openairdocs.org/sdr/CALA2014081501126.md): Frame · cracked · Aug 15, 2014 · N78285 · Boeing 737824 · Fuselage Main, Frame
  > STATION 727B RT, BETWEEN STRINGER 8 & 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME. THE INBD RIVET HOLE HAS A CRACK INDICATION ON THE FRAME. CUT OUT DAMAGE, FABRICATED REPAIR ANGLES FOR FRAME 727B RT, BETWEEN STRINGER 8

Next page: https://openairdocs.org/aircraft/N78285/reports.md?page=2

## 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 = 'N78285' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N78285/reports

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