# Service difficulty reports: N36280

A list on [N36280](https://openairdocs.org/aircraft/N36280.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 · 66 reports

- [SDR CALA2026092819849](https://openairdocs.org/sdr/CALA2026092819849.md): Light · abnormal · Sep 21, 2026 · N36280 · Boeing 737824 · Passenger Compartment Lighting
  > ROW 21DEF EMERGENCY EXIT DOOR FLOURESENT LIGHT IS FLICKERING REQUESTING MEL FOR RT. SIDE WINDOW LIGHTS INOP. RESET NO HELP. C/B PULLED ON P92 E-11 RT WINDOW LTS. VERIFIED EMERG. EXIT LIGHTS WORKING PROPERLY TOMC APPROVED IAW MEL 3302B CONFIRMED EMERGENCY EXIT
- [SDR CALA2026083119086](https://openairdocs.org/sdr/CALA2026083119086.md): Power Supply · faulted · Aug 28, 2026 · N36280 · Boeing 737824 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS ON. DURING T/S, FOUND CB A10, LT AFT EMGER CHARGE, ON P18-3 PANEL HAD POPPED. ALL LT AFT EMERGENCY LIGHTS STARTING WITH OVERWING EXIT TO BACK OF ACFT ARE TURNING ON WITH OVERHEAD EMERGENCY EXIT LIGHTS SWITCH IN ARMED POSITION
- [SDR CALA2026030414301](https://openairdocs.org/sdr/CALA2026030414301.md): Unknown · odor · Mar 4, 2026 · N36280 · Boeing 737824 · Air Distribution System
  > APU HAD A SLIGHT FUEL ODOR WHEN FUNNING PACKS WITH APU AS AIR SOURCE. REQUESTING MEL 4901A. OK TO PLACE APU ON MEL 4901A. CURRENTLY UNABLE TO LOCATE SOURCE ON APU. APU ON MEL FOR SLIGHT FUEL ODOR ON PACK START UP WITH APU AS SOURCE, INSPECTED APU AND BOT
- [SDR CALA2026030314261](https://openairdocs.org/sdr/CALA2026030314261.md): Circuit Breaker · open · Mar 2, 2026 · N36280 · Boeing 737824 · Electrical Power System Wiring
  > NO DUCT PRESSURE ON APU. NO DUAL BLEED LIGHT. REQUESTING PER MEL 4907A. C/W DDP. APPROVED MEL 4907A. APPLIED STICKER. RT A/C PACK OPS TEST NO PRESSURE. PERFORMED BLEED AIR ISOLATION TEST. CLOSED ALL A/C PACK CONTROL AND ISOLATION VALVE CIRCUIT BREAKERS.
- [SDR CALA2026030314214](https://openairdocs.org/sdr/CALA2026030314214.md): Unknown · odor · Mar 2, 2026 · N36280 · Boeing 737824 · Air Distribution System
  > FUMES IN FLT DECK WITH ALL BLEEDS CLOSED. PERFORMED SMOKE CONDITIONAL INSPECTION IAW AMM 05-51-26. NO DEFECTS NOTED. APU OPS CHECKED GOOD IAW 49-11-00. NO FUMES DETECTED DURING STARTING OR OPERATION.
- [SDR CALA2026030314213](https://openairdocs.org/sdr/CALA2026030314213.md): Apu · smoke · Mar 1, 2026 · N36280 · Boeing 737824 · Airborne Auxiliary Power Unit (APU) System
  > APU WILL NOT HOLD ELECTR ICAL POWER, GROUND CREW SAW A PUFF OF SMOKE FROM APU. FUMES IN FLT DECK STARTED APU IAW 49-11-00. VERIFIED NO SMOKE OR FUMES ON START. REMOVED GROUND POWER, APU CONTINUED TO RUN WITH NO ISSUES NO FOUL ODOR DETECTED.
- [SDR CALA2026011212880](https://openairdocs.org/sdr/CALA2026011212880.md): Door · out of adjust · Jan 9, 2026 · N36280 · Boeing 737824 · Passenger/Crew Doors
  > FAS REPORT DOOR 2L QUITE LOUD IN FLIGHT AND LEAKS EXCESSIVE WATER ON GROUND. PRESSURIZED AIRCRAFT TO 4.5 PSI, SPARYED LEAK DECTECTOR FOUND MASSIVE LEAK AT LOWER AFT SIDE OF DOOR INSPECTED DOOR SEALS NO DEFECTS NOTED. ACCOMPLSHED AFT LT ENTRY DOOR ADJUSTMENT/T
- [SDR CALA2025072907047](https://openairdocs.org/sdr/CALA2025072907047.md): Control Switch · faulted · Jul 28, 2025 · N36280 · Boeing 737824 · Engine Thrust Reverser
  > ENG 2 REV THRUST STICKY ON LANDING. PERFORM THE BITE TEST ON 2 ENGINE REV THE EAU FOUND ONLY ONE FAULT T/R DELOY FAULT DID THE NORMAL OPS TEST SYSTEM WORK UNTIL NOTICE AFTER YOU DELOYED THE HANDLE TO FULL DELOY THE T/R DOES NOT DELOY AND YOU GET THE REV LIGHT
- [SDR CALA2025051504686](https://openairdocs.org/sdr/CALA2025051504686.md): Girt Bar · loose · May 14, 2025 · N36280 · Boeing 737824 · Emergency Equipment
  > 1L GIRT BAR NEEDS INSPECTION.FA REPORTS END IS LOOSE L1 DOOR SLIDE GIRT BAR RELEASE STOP COLLAR HALVES SPLIT. INSTALLED NEW GIRT BAR RELEASE STOP ASSEMBLY IAW AMM 25-66-01-400-803.
- [SDR CALA2024122201610](https://openairdocs.org/sdr/CALA2024122201610.md): Smoke Detector · false activation · Dec 20, 2024 · N36280 · Boeing 737824 · Smoke Detection
  > LAV E SMOKE ALARM WENT OFF INTERMITANTLY 3 TIME S WITH NO EVIDEN CE OF SM OKE OR FUMES NO FAULTS NOTED UPON ARRIVAL. PERFORMED BITE OF LAV E SMOKE DET PER AMM26-14-00-710-802. OPS CHECK GOOD. NO HISTORY
- [SDR CALA2024121601524](https://openairdocs.org/sdr/CALA2024121601524.md): Wire · loose · Dec 11, 2024 · N36280 · Boeing 737824 · Light System Wiring
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - ROWS 2ABC,3ABC,4ABC EMERGENCY LIGHTS INOP. FOUND LOOSE WIRES BELOW SEAT TRACK COVER IN WIRE BUNDLE TRACK. ADJ/SECURED WIRES. OPS CHK GOOD. EMERG. LIGHTS WORKING AS DESIGNED. AMM REF 33-51-00
- [SDR CALA2024091000618](https://openairdocs.org/sdr/CALA2024091000618.md): Warning Light · illuminated · Sep 7, 2024 · N36280 · Boeing 737824 · Airspeed/Mach Indicator
  > IAS DISAGREE LIGHT 80KTS CA...95KTS FO PERFORMED FIM 31-62 TASK 876. UPON PERFORMING FLUSHING, AMM TASK 34-11-00-170-802.RETRACTED DEBRIS FROM CAPTAIN'S PITOT LINE.PERFORMED PITOT LEAK CHECK PER AMM TASK 34-11-00-790-810.OPS CHECK GOOD. VERIFIED PITOT TUBES WE
- [SDR CALA2024050101289](https://openairdocs.org/sdr/CALA2024050101289.md): Skin · damaged · Apr 30, 2024 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE ON EXTERNAL SURFACE OF SKIN JUST AFT OF LIVE TV DOUBLER LOCATED AT 727E S-3L. DAMAGED AREA IS APPROXIMATELY 2 1/ 2 INCHED LONG. SEE BAM N/R 001867632 FOR REPAIR OF AREA. READ "ACCOMPLISH INSPECTION REQUIREMENTS OF THE CROWN SKIN EC/RA 5331-03088 O
- [SDR CALA2024050101288](https://openairdocs.org/sdr/CALA2024050101288.md): Skin · dented · Apr 30, 2024 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LIVE TV DOUBLER LOCATED ON EXTERNAL SURFACE AT 727C BETWEEN S-2L AND S-3L IS DIFFERENT THAN WHAT IS SHOWN OF T-CARD T29-4430-1-0057. ALL 3 END FASTENERS AT FWD END ARE UNDER THE DOUBLER SO THE TWO FWD FASTENERS SHOWN ON THE ILLUSTRATION CAN NOT BE HFEC INSPECT
- [SDR CALA2024042401234](https://openairdocs.org/sdr/CALA2024042401234.md): Skin · corroded · Apr 24, 2024 · N36280 · Boeing 737824 · Wing, Plate/Skin
  > L/H WING UPPER SKIN INTERNAL SKIN CORROSION AT WSTA 685 BETWEEN STRINGER 12A-10B WAS REPAIRED ON BAM N/R 001906676 REF EC/RA 5721-01492 AND REQUIRES A SIGNIFICANT FINDINGS REPORT TO NE ISSU ED. CREATED SFR #1035938
- [SDR CALA2024042401233](https://openairdocs.org/sdr/CALA2024042401233.md): Stringer · corroded · Apr 24, 2024 · N36280 · Boeing 737824 · Wing, Longeron/Stringer
  > L/H WING UPPER STRINGER 12A HAS CORROSION AT WSTA 685.
- [SDR CALA2024042201190](https://openairdocs.org/sdr/CALA2024042201190.md): Frame · mechanic error · Apr 19, 2024 · N36280 · Boeing 737824 · Fuselage Main, Frame
  > BS 520 FRAME INNER CORD AT L/H WL 210 HAD A MISDRILLED FASTENER. INNER CHORD AT S-17L, ACCOMPLISH INSPECTION REQUIREMENTS PER 50,000 TOTAL FLIGHT CYCLES." REF EC/RA 5310-08292 REV A PART 1 001876045 FOR ALL WORK ACCOMPLSHED. PART 2 OF EC/RA 5310-08292 ON OR BE
- [SDR CALA2024041501069](https://openairdocs.org/sdr/CALA2024041501069.md): Skin · cracked · Apr 12, 2024 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LEFT HAND SIDE LOWER HORIZONTAL SKIN CRACKED AT STATION 157.10 APROX. 10 INCHES AND 20 INCHES FROM AFT SPAR. EACH CRACK IS ONE INCH IN LENGTH AND MARKED. REF BAM NON-ROUTINE 001864997 FOR COMPLETION OF REPAIR. A DIP IS REQUIRED TO BE ISSUED IAW SRM 55-10-01-2R
- [SDR CALA2024041501068](https://openairdocs.org/sdr/CALA2024041501068.md): Skin · cracked · Apr 11, 2024 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STAB STA 147.90 LOCATED 9 INCHES FWD OF AFT SPAR. CRACK IS MARKED AND MEASURES 1 INCH LONG. REF BAM NON-ROUTINE 001865013 FOR COMPLETION OF RE PAIR. A DIP IS REQUIRED TO BE ISSUED IAW SRM 55-10-01-2R-11 REPA IR 11
- [SDR CALA2024041001014](https://openairdocs.org/sdr/CALA2024041001014.md): Skin · cracked · Apr 9, 2024 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STAB LOWER SKIN HAS 2 CRACKS AT STAB STA 101.90 O NE 10" FWD OF AFT SPAR AND ONE 20" FWD OF AFT SPAR. REF BAM NR 1 865008 AND NR 1865012. 12 ARE COMBINDED INTO ONE REPAIR DOUBLER ON BAM NR 1865008. INSTALLED REPAIR DOUBLER AT STAB STA 101.90 SEE
- [SDR CALA2024040300945](https://openairdocs.org/sdr/CALA2024040300945.md): Structure · corroded · Mar 11, 2024 · N36280 · Boeing 737824 · Fuselage Main, Attach Fittings
  > R2 DOOR CHORD HAS CORROSION ON BOTTOM (MARKED). FROM BAM N/R 001885605. FOR ESFR REPORTING. REF. BAM N/R 001885605 FOR ALL WORK PERFORMED.. REMOVED AND REPLACED R2 CHORD PER SRM 51-10-02 AND SRM 51-40-02. FOR ESFR REPORTING. VERIFIED ESFR C/W.
- [SDR CALA2023101803104](https://openairdocs.org/sdr/CALA2023101803104.md): Unknown · unknown · Oct 17, 2023 · N36280 · Boeing 737824 · Air Distribution System
  > INTERMITENT ELECTRICAL SMELL CAPT SIDE WHILE ENROUTE.CAPT LEFT AND OR BEHIND AREA SUSPECT. DEBRIEFED CREW, F/O DID NOT SMELL ODOR, ONLY CAPTAIN. PERFORMED ELECTRICAL ARCING IN FLIGHT DECK NOR CABIN. CONDITIONAL INSPECTION, SMOKE/ODOR IN FLIGHT DECK/CABIN IAW A
- [SDR CALA2023100402936](https://openairdocs.org/sdr/CALA2023100402936.md): Latch · binding · Oct 1, 2023 · N36280 · Boeing 737824 · Escape Slide
  > L1 DOOR SLIDE DROPPED FROM SHROUD. SLIDE DID NOT DEPLOY. FOUND DOOR SLIDE LATCH ASSY STIFF. REPLACED CHECK OK. END
- [SDR CALA2021092201635](https://openairdocs.org/sdr/CALA2021092201635.md): Pitot Head · none · Sep 21, 2021 · N36280 · Boeing 7378 · Elevator Tab Control System
  > FEEL DIFF PRESS LITE ON ROTATE CLIMB OUT FOUND BUILDUP AT INLET OF RT ELEV PITOT PROBE. CLEANED AND FLUSHED ELEV FEEL PITOT PROBES PER AMM 27-31-17. PERFORMED PRESSURIZATION CHK PER SAME. PRESS READS SAME AND INDICATIONS NORMAL. OK TO CONTINUE.
- [SDR CALA2021063000999](https://openairdocs.org/sdr/CALA2021063000999.md): Skin · cracked · Jun 30, 2021 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK - EA 5510-01843 REV H OP 001 - RH HORIZONTAL STABIL IZER LOWER SKIN PANEL AT STA 129.5 FOUND 1EA CRACK APPROX 0.875" IN LENGTH REF NR LP 9130718 RH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-1-01-2R-11 REPAIR 11 FIG 204 TABLE 201 AND TABLE 203 CA
- [SDR CALA2021063000998](https://openairdocs.org/sdr/CALA2021063000998.md): Skin · cracked · Jun 30, 2021 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK - EA 5510-01843 REV H OP 001 - L/H HORIZONTAL STABI LIZER LOWER SKIN PANEL AT STA 129.5 FOUND 1EA CRACK APPROX 0.875 " IN LENGTH REF NR LP 9130720 LH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-10-01-2R-11 REPAI R 11 FIG 204 TABLE 201 AND TABLE 20
- [SDR CALA2021063000997](https://openairdocs.org/sdr/CALA2021063000997.md): Skin · cracked · Jun 30, 2021 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK - EA 5510-01843 REV H OP 001 - RH HORIZONTAL STABIL IZER LOWER SKIN PANEL AT STA 175.5 FOUND 1EA CRACK APPROX 1.750" IN LENGTH REF NR LP 9130719 RH HORIZONTAL STABILIZER LOWER SKIN REPAIRED AS PER SRM 55-10-01 -2R-11 REPAIR 11 FIG 204 TABLE 202 AN
- [SDR CALA2021063000996](https://openairdocs.org/sdr/CALA2021063000996.md): Skin · cracked · Jun 30, 2021 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK - EA 5510-01843 REV H OP 001 - L/H HORIZONTAL STABI LIZER LOWER SKIN PANEL AT STA 101.9 FOUND 1EA CRACK APPROX 1" IN LENGTH REF NR LP 9130721 LH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-10-01-2R-11 REPAI R 11 FIG 204 TABLE 201 AND TABLE 203 CAT
- [SDR CALA2021011100034](https://openairdocs.org/sdr/CALA2021011100034.md): Restrictor Valve · obstructed · Jan 9, 2021 · N36280 · Boeing 737824 · Aileron Control System
  > FEEL DIFF PRESS LIGHT, PER FLIGHT CREW FEEL DIFF LIGHT EXTINGUISHED AFTER LANDING. PERFORMED FIM TASK 27-31-00-810-815 STEP E(7). CLEANED DEBRIS FROM LT ELEVATOR RESTRICTOR VALVE. UNABLE TO COMPLETE ISLOLATION PROCEDURE "C" LIFT EQUIP UNAVAILABLE 1-00-700-8
- [SDR CALA2020070401035](https://openairdocs.org/sdr/CALA2020070401035.md): Switch · open · Jul 1, 2020 · N36280 · Boeing 737824 · Landing Gear Position and Warning
  > AIR RETURN FLIGHT 2859 MNL. ALL LANDING GEAR WOULD NOT RETRACT. ALL GREEN LIGHTS (6) AND ALL RED LIGHTS (3) ON WHEN GEAR HANDLE WAS SELECTED UP, VERBAL FROM CREW. CYCLED HANDLE DOWN AND LANDED NORMAL. PERFORMED BITE OF PSEU NO FAULTS, NO FAILURES. FIM 32-0
- [SDR CALA2020053100994](https://openairdocs.org/sdr/CALA2020053100994.md): Pin · worn · May 23, 2020 · N36280 · Boeing 737824 · Flight Compartment Windows
  > UNABLE TO ACCESS COCKPIT USING EXTERNAL FIRST OFFICERS WINDOW EMERGENCY RELEASE HANDLE. NO AMOUNT OF PULLING RELEASES WINDOW. AFTER FURTHER EVALUATION FOUND CAMSHAFT PIN WORN. R & R CAM PIN ASSEMBLY & AMP. PERFORMED EMERGENCY EXIT RELEASE ADJUSTMENT IAW AM
- [SDR CALA2020041000820](https://openairdocs.org/sdr/CALA2020041000820.md): Power Supply · inoperative · Apr 8, 2020 · N36280 · Boeing 737824 · Emergency Lighting
  > SEAT ROW 30 AND 34 ABC AND L2 DOOR EMERGENCY LIGHT INOP REMOVE AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK (M1673) AT LEFT AFT CABIN CEILING STA 952 WL 290 LBL 14 PER AMM 33-51-06
- [SDR CALA2019031500414](https://openairdocs.org/sdr/CALA2019031500414.md): Warning System · false activation · Mar 14, 2019 · N36280 · Boeing 737824 · Landing Gear Position and Warning
  > AFTER T/O GEAR LEVER UP ALL 3 GEAR INDICATONS SHOWED RED AND GREEN LIGHTS. GEAR NOT RTRCTD PERFORMED FIM TASK 32-30-00-810-805. OPS CK SEVERAL TIMES, NO FAULTS NOTED. A/C OK FOR SVC -END- RII INSPECTION C/W PER GMM 09-25-05.
- [SDR CALA2018091701939](https://openairdocs.org/sdr/CALA2018091701939.md): Fitting · corroded · Sep 13, 2018 · N36280 · Boeing 737824 · Service Doors
  > R1 DOOR STOP PIN FITING THIRD FROM TOP HAS CORROSION. REMOVED AND REPLACED FITTING PER SRM 51-40-02 AND DWG 141 A6516.
- [SDR CALA2018090701908](https://openairdocs.org/sdr/CALA2018090701908.md): Skin · cracked · Sep 6, 2018 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZ STAB LWR SKIN HAS 1.5" CRACK AT STAB STA 129.50, 27" FROM STAB FRONT SPAR. REPAIRED LOWER STAB SKIN AS REF SRM 55-10-01 REPAIR 11.
- [SDR CALA2018083101868](https://openairdocs.org/sdr/CALA2018083101868.md): Skin · cracked · Aug 30, 2018 · N36280 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORZ STAB LWR SKIN HAS 2 EA CRACK AT STAB SKIN STA 129.50 THE FIRST CRACK IS 1.25 LONG 27 INCHES FROM STAB FRONT SPAR AND THE SECOND CRACK IS 1.25 LONG 35 INCHES FROM FRONT SPAR. REPARED STAB SKIN REF SRM 55-10-01 REF FLEETCYCLE L/P 9614041 FOR WORK PERFORM
- [SDR CALA2017102303760](https://openairdocs.org/sdr/CALA2017102303760.md): Fitting · loose · Oct 23, 2017 · N36280 · Boeing 737824 · Emergency Equipment
  > GIRT BAR CLIP ON SLIDE PACK HOUSING LOOSE AT DOOR 2L. ADJUSTED GIRT BAR CLIP. NO DEFECTS NOTED,.
- [SDR CALA2017091103130](https://openairdocs.org/sdr/CALA2017091103130.md): Circuit Breaker · open · Sep 11, 2017 · N36280 · Boeing 737824 · Engine Control System Wiring
  > REVERSE THRUST LEVER HAS LOST MOTION, NO THRUST REVERSER OPERATION FOR NR 2 ENGINE, FOUND CIRCUIT BREAKERS OUT AT GATE. NR 2 ENGINE SYNC LOCK, INTLK, CONT, AND IND. RESET. NR 2 THRUST REVERSER OPS CHECKED OK, NO FAULTS NOTED.
- [SDR CALA2017090403043](https://openairdocs.org/sdr/CALA2017090403043.md): Bezel · burned · Sep 4, 2017 · N36280 · Boeing 737824 · Passenger Compartment Lighting
  > FLT ATTENDANT REPORTED A BRIEF MOMENT OF SMOKE, BOTH VISUALLY AND BY SMELL FROM FORWARD GALLEY, SPOKE WITH FLIGHT CREW, FO COULD DETECT THE SMOKE AND FLT ATTENDANT ALSO AROUND FIRST CLASS GALLEY, WHITE SMOKE WAS NOTED AT TOP END OF GALLEY FOR A SHORT TIME.
- [SDR CALA2017020300255](https://openairdocs.org/sdr/CALA2017020300255.md): Lens · loose · Feb 3, 2017 · N36280 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN DOES NOT TURN OFF. OVERWING EXIT SIGN FALLING OFF ACTUAL PROBLEM IS AISLE CENTER EMERG EXIT SIGN LENS LOOSE. REATTACHED AND SECURED LENS.
- [SDR CALA2016120901059](https://openairdocs.org/sdr/CALA2016120901059.md): Battery · inoperative · Dec 9, 2016 · N36280 · Boeing 737824 · Emergency Equipment
  > AFT GALLEY EMERG FLASHLIGHT INDICATOR NOT FLASHING. REPLACED THE BATTERY.
- [SDR CALA2015042800330](https://openairdocs.org/sdr/CALA2015042800330.md): Flap · malfunctioned · Apr 24, 2015 · N36280 · Boeing 737824 · Trailing Edge Flap Control System
  > ON FINAL APPROACH, WIND GUST EXCEEDED FLAPS 30 SPD & THEY RETRACTED TO 25, ON MISSED APPROACH THEY WERE LOCKED OUT AT ABOUT 27 COULD NOT RETRACT, FLAP STAYED AT 27 UNTIL LANDING & RETURNED TO 25 AFTER TOUCHDOWN. MAX SPEED ON MISS WAS 195 WITH GUSTS & FLAP AT
- [SDR CALA2015030900147](https://openairdocs.org/sdr/CALA2015030900147.md): Battery Pack · discharged · Mar 6, 2015 · N36280 · Boeing 737824 · Emergency Lighting
  > EMERGENCY BATTERY PACK FOR LT WING EMER LIGHTS INOPERATIVE. SEE WORK ACCOMPLISHED ON NR 6174406. R & R EMER EXIT LIGHT BATTERY PACK M1694 IAW AMM 33-51. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.
- [SDR CALA2015030900145](https://openairdocs.org/sdr/CALA2015030900145.md): Battery Pack · discharged · Mar 5, 2015 · N36280 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK FWD LT EMER PATH LIGHT INOPERATIVE AT STATION 322, WL 291 & RBL 7. R & R BATTERY PACK M1674 IAW MM 33-51-06. OPERATIONAL CHECKED GOOD PN AD-D 717-01-100.
- [SDR CALA2015030900144](https://openairdocs.org/sdr/CALA2015030900144.md): Battery Pack · discharged · Mar 5, 2015 · N36280 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK EMER LIGHT OUTSIDE L1 ENTRY DOOR INOPERATIVE, STATION 322. R & R EMER LIGHT BATTERY PACK. OPERATIONAL CHECKED GOOD IAW AMM 33-51-06. PN AD-D717-01-100.
- [SDR CALA2015030900143](https://openairdocs.org/sdr/CALA2015030900143.md): Battery Pack · discharged · Mar 5, 2015 · N36280 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK EMER LIGHTS ABOVE RT WING INOPERATIVE, STATION 565, WL 213 & RBL 68. REMOVED EMER EXIT LIGHT BATTERY PACK M1695 FOR RT OVERWING & INSTALLED NEW EMER BATTERY PACK IAW AMM 33-51-06. OPERATIONS CHECKED GOOD. MANUFACTURER PN ADD717-01-100 BN 156305
- [SDR CALA2015030400140](https://openairdocs.org/sdr/CALA2015030400140.md): Skin · damaged · Mar 4, 2015 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SUPPORT TASK GEN N/ TO CAPTURE ADDITIONAL WORK FROM ORIGINATING NR 6167014. REMOVED DAMAGED SKIN, FABRICATED & INSTALLED FILLER & DOUBLER IAW ECRA 5330-05083 REV.
- [SDR CALA2013091800681](https://openairdocs.org/sdr/CALA2013091800681.md): Skin · gouged · Sep 16, 2013 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, FWD OF AFT LT DOUBLER, BETWEEN STATION 727D & AMP STATION 727E 3 INCHES TO THE LT OF STRINGER 2L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3
- [SDR CALA2013091800680](https://openairdocs.org/sdr/CALA2013091800680.md): Skin · gouged · Sep 16, 2013 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, JUST OTBD OF LT DOUBLER, STATION 727E AT STRINGER 3L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3L.
- [SDR CALA2013091800679](https://openairdocs.org/sdr/CALA2013091800679.md): Skin · gouged · Sep 16, 2013 · N36280 · Boeing 737824 · Fuselage Main, Plate/Skin
  > UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, JUST OTBD OF LT DOUBLER, 2 INCHES FWD OF STATION 727E AT STRINGER 3L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3L.

Next page: https://openairdocs.org/aircraft/N36280/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 = 'N36280' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N36280/reports

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