# Service difficulty reports: Boeing 737-36N

A list on [Boeing 737-36N](https://openairdocs.org/model/boeing-737-36n.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 53 reports

- [SDR 2026F00172](https://openairdocs.org/sdr/2026F00172.md): Windshield · cracked · Jul 31, 2026 · Boeing 73736N · Flight Compartment Windows
  > FLIGHT 650 CBB-VVI CRACKED WINDOW #R1 DURING DESCENT. CORRECTIVE ACTION: REMOVED AND REPLACED WINDOW #1 AND CHANGED CONTROL CABIN WINDOW HEAT. IN TEST NORMAL
- [SDR 2025F00017](https://openairdocs.org/sdr/2025F00017.md): Battery · discharged · Jan 4, 2025 · Boeing 73736N · Battery/Charger System
  > BOTH DC FAIL. LIGHTS ILLUMINATED. LOW BATTERY VOLTAGE. CANCELLED AIRCRAFT IN SLVR. CORRECTIVE ACTION: REMOVED AN REPLACED MAIN BATTERY
- [SDR 2024F00268](https://openairdocs.org/sdr/2024F00268.md): Control System · failed · Oct 31, 2024 · N836CC · Boeing 73736N · Fuel Control/Turbine Engines
  > CANCELED FLIGHT 646 CBB/VVI DUE TO ENGINE #2 SLOW ACCELERATION IN DIFFERENTE PHASES OF FLIGHT AND HOT STARTS. CORRECTIVE ACTION: REMOVED AN INSTALLED MAIN ENGINE CONTROL MEC.
- [SDR 2024F00183](https://openairdocs.org/sdr/2024F00183.md): Tire · failed · Jul 30, 2024 · N836CC · Boeing 73736N · Tire
  > TIRE#2 TREAD LOSS. CANCELLED AIRCRAFT LEG CBB/TDD FLIGHT 466. CONDITIONAL INSPECTION PERFOMED. FOUND DAMAGE IN FLAP I NLEFT INBOARD FORE FLAP WITHIN LIMITS. LEFT INBOARD AFT FLAP REMOVED AND REPLACED
- [SDR 2024F00029](https://openairdocs.org/sdr/2024F00029.md): A/C Pack · tripped · Feb 5, 2024 · Boeing 73736N · Cabin Cooling System
  > QRF TO VVI DUE TO PACK TRIP OFF#2 LIGHT ILLUMINATE AFTER TAKE OFF. CORRECTIVE ACTION: PERFORMED ADJUSTMENT/TEST IAW AMM 21-51-00/501 SYST WORK PROPERLY ON GROUND WITH POWER PLANT TEST.
- [SDR 2023F00010](https://openairdocs.org/sdr/2023F00010.md): Fitting · corroded · Dec 3, 2022 · N836CC · Boeing 73736N · Fuselage, Landing Gear Attach Fittings
  > MLG LH AND RH LUG FITTINGS WITH CORROSION DAMAGE LEFT SIDE: 0.070" AND 11HRS; 0.044" AT 10HRS; 0.049" AT 12HRS. RIGHT SIDE: 0.069" AT 12HRS,0.057" AT 11HRS.
- [SDR 2022F00227](https://openairdocs.org/sdr/2022F00227.md): Motor · failed · May 16, 2022 · Boeing 73736N · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP ASSYMETRY DURING TKEOFF, FLAPS ON THE RIGHT WING STUCK ON 1 AND FLAPS ON THE LEFT WING WENT UP. CORRECTIVE ACTION: HAS BEEN CHANGED FLAP HYDRAULIC MOTOR IAW AMM 27-51-57/401 AND TE FLAP BYPASS VALVE IAW AMM 27-52-82/401 AND PERFORMED OPERATI
- [SDR 2022F00232](https://openairdocs.org/sdr/2022F00232.md): None · none · May 8, 2022 · Boeing 73736N · Passenger/Crew Doors
  > STRONG NOISE AND VIBRATION DOOR 1L. CORRECTIVE ACTION:HAS BEEN CHANGED DOOR 1L IAW AMM 52-11-00/401 AND ADJUSTED TEST NORMAL IAW AMM 52-11-00/501
- [SDR 2022F00127](https://openairdocs.org/sdr/2022F00127.md): None · none · Mar 14, 2022 · Boeing 73736N · Fuselage Main, Longeron/Stringer
  > CRACKING ON STA 291.5 FRAME WEB - INTERCOSTAL STRAT CUTOUT AT STRINGER 14R. CRACKING ON STA 277 INTERCOSTAL - STRINGER 16R RADIUS TRIMOUT. THESE CRACKINGS WERE FOUND AS PER AD 2014-22-06
- [SDR 2022F00009](https://openairdocs.org/sdr/2022F00009.md): Relay · blocked · Nov 7, 2021 · Boeing 73736N · Landing Gear Retraction/Extension System
  > LANDING GEAR LEVE WILL NOT MOVE UP AFTER TAKEOFF. LANDING GEAR DOWN, THERE IS NO ANY GREEN LIGHT INDICATORS
- [SDR UIEA2021072201607](https://openairdocs.org/sdr/UIEA2021072201607.md): Flap · damaged · Jun 28, 2021 · N1093A · Boeing 73736N · Trailing Edge Flaps
  > MULTIPLE AREAS OF DAMAGE ON LH IB FLAP ASSY, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02. CUSTOMER REQUEST FLAP REPLACEMENT. REMOVED AND REPLACED LH IB FLAP ASSY AND OPS CHECK GOOD IAW B767 AMM 27-51-06-422-059.
- [SDR CA1912050006](https://openairdocs.org/sdr/CA1912050006.md): Adapter · failed · Jan 24, 2016 · Boeing 73736N · Glide Slope System
  > (CAN) FINAL APPROACH CONDUCTING LPV APPROACH AIRCRAFT WAS FULLY CONFIGURED AND STABLE ON APPROACH WITH LOCALIZER AND GLIDE SLOPE CAPTURED. EXACTLY WHILE CROSSING FAF GLIDE SLOPE HAD A LARGE UPWARD DEVIATION AND AUTOPILOT RAPIDLY PITCHED AIRCRAFT NOSE UP. I IMM
- [SDR CA140627001](https://openairdocs.org/sdr/CA140627001.md): Mechanism · stiff · Jun 26, 2014 · Boeing 73736N · Aileron Control System
  > (CAN) PILOT REPORTED: F/O YOKE FEELS STIFF DURING CONTROL CHECK. ONLY STIFF WITH LT AILERON, F/O SIDE. FOUND STIFFNESS AND NOISE EMANATING FROM AILERON TRANSFER CONTROL MECHANISM ASSY. MECHANISM ASSEMBLY REPLACED.
- [SDR 7AHR201404152372](https://openairdocs.org/sdr/7AHR201404152372.md): Floor Support · corroded · Apr 11, 2014 · N558MS · Boeing 73736N · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STRUCTURE AT LBL 14.00 AT STA 727A, 727D, 747, 787 AND 847 CARGO TIE DOWN FITTINGS CORRODED. REMOVED CORROSION ON FITTINGS AND FABRICATED NEW SECTION OF CARGO TRACK THAT WAS OUT OF LIMITS IAW SRM 51-40-02, PGS 2, 3 & 4.
- [SDR 7AHR201404152449](https://openairdocs.org/sdr/7AHR201404152449.md): Floorbeam · corroded · Apr 10, 2014 · N558MS · Boeing 73736N · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT BS 994, LBL 33-44 CORRODED. REMOVED CORROSION IN AREA AND REPAIRED IAW SRM 51-40-02.
- [SDR 7AHR201404152522](https://openairdocs.org/sdr/7AHR201404152522.md): Floor Support · corroded · Apr 10, 2014 · N558MS · Boeing 73736N · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CHANNEL HAS CORROSION AT BS 956, RBL 50. REMOVED CORROSION, FABRICATED FLOOR SUPPORTS AND INSTALLED IAW SRM 51-10-07 AND 53-40-02.
- [SDR 7AHR201404152462](https://openairdocs.org/sdr/7AHR201404152462.md): Floorbeam · corroded · Apr 10, 2014 · N558MS · Boeing 73736N · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM HAS CORROSION AT BS 867, BL 0. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-00-07, FIG 202, PGS 208-214.
- [SDR 7AHR201404152451](https://openairdocs.org/sdr/7AHR201404152451.md): Frame · corroded · Apr 10, 2014 · N558MS · Boeing 73736N · Fuselage Main, Frame
  > RIGHT FUSELAGE FRAME AT BS 994, RBL 48 HAS CORROSION ON FWD & INBD SIDE OF FRAME. REMOVED CORROSION AND INSTALLED REPAIR TO FRAME IAW SRM 56-60-15 & 51-40-05.
- [SDR 7AHR201404152335](https://openairdocs.org/sdr/7AHR201404152335.md): Frame · corroded · Apr 9, 2014 · N558MS · Boeing 73736N · Fuselage Main, Frame
  > AFT CARGO BAY, FRAME BS 747 BETWEEN S28L & 27R CORRODED. REMOVED CORROSION FROM AREAS, REPAIRED IAW SRM 53-00-07, FIG 201.
- [SDR 7AHR201404152532](https://openairdocs.org/sdr/7AHR201404152532.md): Seat Track · corroded · Apr 9, 2014 · N558MS · Boeing 73736N · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 390, RBL 45. R & R SECTION OF SEAT TRACK IAW SRM 53-00-52.
- [SDR 7AHR201404152106](https://openairdocs.org/sdr/7AHR201404152106.md): Intercostal · cracked · Apr 8, 2014 · N558MS · Boeing 73736N · Trailing Edge Flaps
  > LEFT INBD MIDFLAP INTERCOSTAL INBD END OF OTBD TORQUE TUBE IS CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02. INTERCOSTAL FABRICATED IAW DWG 57-14105-01, REV NEW. INSTALLED INTERCOSTAL IAW SRM 51-40-02.
- [SDR 7AHR201404082448](https://openairdocs.org/sdr/7AHR201404082448.md): Floorbeam · corroded · Apr 8, 2014 · N558MS · Boeing 73736N · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUTPLATE HOLES FROM RBL 4-44 UPPER CAP. INSTALLED REPAIR IAW SRM 53-60-51.
- [SDR 7AHR201404082445](https://openairdocs.org/sdr/7AHR201404082445.md): Floor Support · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT AT BS 967 LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-60-51.
- [SDR 7AHR548B2444](https://openairdocs.org/sdr/7AHR548B2444.md): Floor Support · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT AT BS 952, LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-2.
- [SDR 7AHR201404082442](https://openairdocs.org/sdr/7AHR201404082442.md): Floorbeam · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM HAS CORROSION BS 948, RBL 4. REMOVED CORROSION AND INSTALLED REPAIR TO IAW SRM 53-30-51, REPAIR 2.
- [SDR 7AHR201404082374](https://openairdocs.org/sdr/7AHR201404082374.md): Striker · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SURROUND STRUCTURE AFT EDGE BS 490 LOWER AFT DOOR STOP HAS BROKEN STRIKER PLATE AND FITTING IS CORRODER. R & R STRIKER PLATE AND FITTING IAW SRM 51-40-02.
- [SDR 7AHR201404082339](https://openairdocs.org/sdr/7AHR201404082339.md): Frame · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Main, Frame
  > AFT CARGO BAY FRAME AT BS 807 HAS CORROSION FROM STRINGER 27L - 28RT. REMOVED CORROSION IAW SRM 53-00-07, FIG 207, REPAIR 17.
- [SDR 7AHR201404082334](https://openairdocs.org/sdr/7AHR201404082334.md): Shear Tie · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 727E SHEAR TIE HAS CORROSION BETWEEN STRINGERS 27-28RT. REMOVED CORROSION AND FABRICATED NEW SHEAR TIE IAW SRM 53-00-07, FIG 202, REPAIR 17.
- [SDR 7AHR201404082288](https://openairdocs.org/sdr/7AHR201404082288.md): Intercostal · corroded · Apr 8, 2014 · N558MA · Boeing 73736N · Fuselage Miscellaneous Structure
  > FWD CARGO BAY INTERCOSTAL BS 420-440 RT HAS DOUBLE DRILLED HOLES AND CORROSION. R & R IAW SRM 53-30-04, FIG 1 AND 51-40-02.
- [SDR F3LA200500011](https://openairdocs.org/sdr/F3LA200500011.md): Roller · worn · Mar 8, 2005 · N306FL · Boeing 73736N · Service Doors
  > MAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE PER MM 25-61-35. REMOVED AND REINSTALLED R1 DOOR LINER PER MM 52-41-31. REMOVED AND REINSTALLED R
- [SDR F3LA200300191](https://openairdocs.org/sdr/F3LA200300191.md): Actuator · inoperative · Dec 31, 2003 · N306FL · Boeing 73736N · Leading Edge Slat Actuator
  > DURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOCK PIN TEST AND LE SLAT ALTERNATE SYSTEM TESTS IAW TASK CARD 5-2710 AND MM 27-81-00.
- [SDR F3LA200300190](https://openairdocs.org/sdr/F3LA200300190.md): Skin · dented · Dec 31, 2003 · N306FL · Boeing 73736N · Fuselage Main, Plate/Skin
  > DURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202.
- [SDR F3LA200300188](https://openairdocs.org/sdr/F3LA200300188.md): Flap Track · corroded · Dec 19, 2003 · N306FL · Boeing 73736N · Trailing Edge Flaps
  > DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRACK PER OHM 57-53-15. MACHINED THE HOLE FORWARD OF BUSHING NR 60 PER SOPM 20-10-01 AND SOPM 20-10-
- [SDR F3LA200300187](https://openairdocs.org/sdr/F3LA200300187.md): Battery Pack · failed · Dec 19, 2003 · N306FL · Boeing 73736N · Escape Slide
  > DURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE.
- [SDR F3LA200300186](https://openairdocs.org/sdr/F3LA200300186.md): Intercostal · cracked · Dec 19, 2003 · N306FL · Boeing 73736N · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOSTAL PER SRM 51-40-2.
- [SDR F3LA200300185](https://openairdocs.org/sdr/F3LA200300185.md): Oxygen Bottle · discharged · Dec 19, 2003 · N306FL · Boeing 73736N · Passenger Oxygen System
  > DURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-22-11, PAGE 401, STEPS 1-3.
- [SDR F3LA200300184](https://openairdocs.org/sdr/F3LA200300184.md): Module · faulty · Dec 19, 2003 · N306FL · Boeing 73736N · Fire Detection
  > DURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G-7 OF FIRE WARNING SYSTEM TEST. TEST 1 G-10 PASSED. REPLACED FIRE DETECTION MODULE PER MM 26-10-01
- [SDR F3LA200300183](https://openairdocs.org/sdr/F3LA200300183.md): Frame · cracked · Dec 19, 2003 · N306FL · Boeing 73736N · Fuselage Main, Frame
  > DURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1-10.
- [SDR F3LA200300182](https://openairdocs.org/sdr/F3LA200300182.md): Shear Tie · corroded · Dec 19, 2003 · N306FL · Boeing 73736N · Fuselage Main, Structure
  > DURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07.
- [SDR F3LA200300181](https://openairdocs.org/sdr/F3LA200300181.md): Shear Tie · corroded · Dec 19, 2003 · N306FL · Boeing 73736N · Fuselage Main, Structure
  > DURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07.
- [SDR F3LA200200394](https://openairdocs.org/sdr/F3LA200200394.md): Strap · corroded · Dec 5, 2002 · N306FL · Boeing 73736N · Fuselage Miscellaneous Structure
  > DURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FILLER/STRAP PER SRM 51-40-02 AND 51-10-02.
- [SDR F3LA200200393](https://openairdocs.org/sdr/F3LA200200393.md): Strap · corroded · Dec 5, 2002 · N306FL · Boeing 73736N · Fuselage Miscellaneous Structure
  > DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED SILL STRAP PER SRM 51-40-07 AND 51-10-02.
- [SDR F3LA200200392](https://openairdocs.org/sdr/F3LA200200392.md): Web · corroded · Dec 5, 2002 · N306FL · Boeing 73736N · Fuselage Miscellaneous Structure
  > DURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40-02 AND 51-10-02.
- [SDR F3LA200200391](https://openairdocs.org/sdr/F3LA200200391.md): Angle · corroded · Dec 3, 2002 · N306FL · Boeing 73736N · Fuselage Miscellaneous Structure
  > DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIRED ANGLE PER SRM 51-40-02, 51-40-05 AND 51-10-02.
- [SDR F3LA200200396](https://openairdocs.org/sdr/F3LA200200396.md): Support Angle · gouged · Dec 3, 2002 · N306FL · Boeing 73736N · Auxiliary Power Unit (APU) Doors
  > DURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 51-70-11. ALODINED AND PRIMED PER MM 51-21-41 AND SOPM 20-41-02. INSTALLED NEW ANGLE PER SRM 52-40
- [SDR F3LA200200395](https://openairdocs.org/sdr/F3LA200200395.md): Cowl Door · chafed · Dec 3, 2002 · N306FL · Boeing 73736N · APU Cowling/Containment
  > DURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITIONAL DAMAGE FOUND AT EDGE OF PREVIOUS REPAIR. FABRICATED NEW DOUBLER TO ENCOMPASS NEW CUTOUT IN SKIN PER SRM 52-40-02, 52-40-01, MM 51-21-41
- [SDR F3LA200200250](https://openairdocs.org/sdr/F3LA200200250.md): Shutoff Valve · failed · Aug 21, 2002 · N306FL · Boeing 73736N · Pneumatic Distribution System
  > AIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, WHICH DECREASED TO 5 PSI WHEN THRUST LEVER REDUCED IN POWER. SHUT DOWN NR 2 ENGINE AND MONITORE
- [SDR F3LA200100123](https://openairdocs.org/sdr/F3LA200100123.md): Wire · broken · Nov 25, 2001 · N306FL · Boeing 73736N · Light System Wiring
  > PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER STANDARD PRACTICES 20-30-12, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM AND CHECKED OKAY.
- [SDR F3LA200000277](https://openairdocs.org/sdr/F3LA200000277.md): Fitting · corroded · Dec 28, 2000 · N306FL · Boeing 73736N · Lavatories
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND RT. AFT LAVATORY OTBD AFT FLOOR MOUNT. MAINTENANCE FABRICATED AND REPLACED NEW FITTING PER EA 25-737-108.
- [SDR F3LA99050](https://openairdocs.org/sdr/F3LA99050.md): Battery · discharged · May 19, 1999 · N306FL · Boeing 73736N · Escape Slide
  > DEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X)

Next page: https://openairdocs.org/model/boeing-737-36n/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 aircraft_model_key = '73736N'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-36n/reports

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