# Service difficulty reports: Boeing 737-2Q9

A list on [Boeing 737-2Q9](https://openairdocs.org/model/boeing-737-2q9.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 250 reports

- [SDR DHL2005741504](https://openairdocs.org/sdr/DHL2005741504.md): Torque Box · cracked · Apr 14, 2005 · N741DH · Boeing 7372Q9 · Fuselage Miscellaneous Structure
  > LT LOWER TORQUE BOX CRACKED AT BS 1213 IN AFT STAIR WELL. REMOVED EXISTING FASTENERS IN AREA AND CUT OUT DAMAGED SECTION (1 IN BY 1 IN) IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER 7075-T6.032 PO NR 900878 (5 1/2 INCH BY 2 1/2 INCH), FILLER 7075-T6.025 7
- [SDR DHL2005741503](https://openairdocs.org/sdr/DHL2005741503.md): Torque Box · cracked · Apr 14, 2005 · N741DH · Boeing 7372Q9 · Fuselage Miscellaneous Structure
  > RT LOWER TORQUE BOX CRACKED IN AFT AIR STAIR WELL AT BS 1225. STOP DRILLED CRACK (.250) IAW B727 SRM 51-10-1. FABRICATED DOUBLER 7075-T6,.032 PO NR 209041(5 INCH BY 3 INCH) IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AN PRIMED AREA AND PART IAW B
- [SDR DHL2005740542](https://openairdocs.org/sdr/DHL2005740542.md): Seat Track · damaged · Mar 29, 2005 · N740DH · Boeing 7372Q9 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BS 760 - BS 870 RBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK BS 760 - 870 RBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-841 PO NR 9001690 DIM 4 FT AND P/N BAC1520-841 PO NR 9001474 DIM. 4 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-
- [SDR CA050125010](https://openairdocs.org/sdr/CA050125010.md): Skin · cracked · Jan 22, 2005 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) AN OUTER FUSELAGE CRACK WAS DISCOVERED AT STRINGER S-18R, STATION 750, APPROXIMATELY 1.125 INCHES LONG. THE CRACK WAS REPAIRED IAW SRM 53-30-3 FIGURE 48, DETAIL IX AND DETAIL XIX.
- [SDR CA050111001](https://openairdocs.org/sdr/CA050111001.md): Gusset · cracked · Jan 5, 2005 · Boeing 7372Q9 · Nose/Tail Landing Gear Attach Section
  > (CAN) DURING A ROUTINE PHASE 3 CHECK (137.5 HRS.), A 2.75 INCH CRACK WAS FOUND ON THE NOSE LANDING GEAR GUSSET WHILE CARRYING OUT SERVICE DIFFICULTY ALERT AL-2002-03.RETRACT ACTUATOR SUPPORT FITTING GUSSET REPLACED IAW SRM 51-30-2 FIG II. TIMES. 61981.7 CYCLES
- [SDR CA041203006](https://openairdocs.org/sdr/CA041203006.md): Skin · cracked · Nov 28, 2004 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) AN OUTER FUSELAGE CRACK WAS FOUND AT STR 16 LT BETWEEN STA 767 & 787 APPROX 2 INCHES LONG. FUSELAGE CRACK REPAIRED IAW SRM 53-30-1 FIG.48 PROCEDURES I, IV & VII. THIS REPAIR IS TIME LIMITED UNTIL 25 FEB. 04. TIMES- 61761:52 CYCLES- 57769.
- [SDR CA041117005](https://openairdocs.org/sdr/CA041117005.md): Engine · failed · Nov 16, 2004 · Boeing 7372Q9 · Engine (Turbine/Turboprop)
  > DURING DAILY CHECK, OIL WAS FOUND IN TAILPIPE AND LAST TWO STAGES OF TURBINE SECTION COATED WITH OIL. RT ENGINE SER NR 667210. RT ENGINE REPLACED. ENGINE SER NR ON 667217. TIMES 61700.25 CYCLES 57721.
- [SDR CA041108010](https://openairdocs.org/sdr/CA041108010.md): Skin · cracked · Nov 6, 2004 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) FUSELAGE CRACK FOUND ON OUTER SKIN AT STN 767 STR 18L, 0.875 INCHES LONG. CRACK REPAIRED IAW SRM 53-30-3 FIG 48 SHEET 32 DETAIL X REV.90. TIMES 61643.42 CYCLES 57682.
- [SDR CA040419002](https://openairdocs.org/sdr/CA040419002.md): Control Cable · chafed · Apr 13, 2004 · Boeing 7372Q9 · Engine Thrust Reverser
  > (CAN) DURING C-CHECK, THE LT ENGINE THRUST LEVER CONTROL CABLE (T1A) WAS FOUND TO BE CHAFED AND HAD BROKEN CABLE STRANDS. DURING INSTALLATION OF NEW CABLE, IT WAS FOUND THAT THE T1A CABLE HAD BEEN ROUTED UNDER THE CABLE GUARD INSTEAD OF OVER, CONTRIBUTING TO
- [SDR CA030918007](https://openairdocs.org/sdr/CA030918007.md): Skin · cracked · Sep 16, 2003 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) DURING ROUTINE DAILY CHECKS A CRACK WAS FOUND ON THE EXTERIOR FUSELAGE AT STN 935-937 STRINGER 24L. CRACK WAS REPAIRED IAW SRM 53-30-3 FIG 48 SHEET 29 DETAIL VI. ACFT TIMES 58839.13 ACFT CYCLES 55678.
- [SDR CA030520003](https://openairdocs.org/sdr/CA030520003.md): Wire · burned · May 16, 2003 · Boeing 7372Q9 · Flight Control System Wiring
  > (CAN) FIVE WIRES DAMAGED FROM ARCING, AT WIRE CLAMP LOCATED OUTBOARD OF NR 2 SLAT OUTBOARD ATTACH ARM AT LT WING STATION 480. NO EVIDENCE OF RUBBING OR CHAFING.WIRE BUNDLE CLAMPS FOUND TO BE IN COMPLIANCE WI TH AD CF-84-08R2. SUSPECT BRITTLE WIRING DUE AGE OF
- [SDR CA030409018](https://openairdocs.org/sdr/CA030409018.md): Skin · cracked · Apr 3, 2003 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) 2.5 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 733 AT STRINGER S-17R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.25. TIMES - 57548:02 CYCLES- 54795
- [SDR CA030409017](https://openairdocs.org/sdr/CA030409017.md): Skin · cracked · Apr 3, 2003 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) 1.7500 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 767 AT STRINGER S-18R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.1 TIMES -57548:02CYCLES -54795
- [SDR TSAA0356043](https://openairdocs.org/sdr/TSAA0356043.md): Windshield · cracked · Mar 7, 2003 · N809AL · Boeing 7372Q9 · Flight Compartment Windows
  > THE CAPTAIN'S FORWARD WINDSHIELD CRACKED WHILE CRUISING AT FL350. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS FORWARD WINDSHIELD. GROUND OPERATIONAL AND PRESSURIZATION CHECKS
- [SDR DHL2003740516](https://openairdocs.org/sdr/DHL2003740516.md): Frame · cracked · Feb 4, 2003 · N740DH · Boeing 7372Q9 · Fuselage Main, Frame
  > UPPER MAIN DECK CARGO DOOR FUSELAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACHED TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABBED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6.050 PER SRM 53-10-4 FIG 11. PARTS TREATED AND DRILLED PER SRM 51-10-2. INSTALLED R
- [SDR CA030120008](https://openairdocs.org/sdr/CA030120008.md): Line · chafed · Jan 16, 2003 · Boeing 7372Q9 · Engine Fuel Distribution
  > (CAN) NR 1 ENGINE FUEL LINE FROM FUEL CONTROL UNIT TO FUEL FLOW TRANSMITTER CHAFING ON TOP OF MAIN OIL TANK. FUEL LINE AND OIL TANK REPLACED. 57134.39 HOURS. 54518 CYCLES.
- [SDR CA021015007](https://openairdocs.org/sdr/CA021015007.md): Skin · cracked · Oct 11, 2002 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STATION 727A & 727B AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30-3 FIG 48.
- [SDR CA021015006](https://openairdocs.org/sdr/CA021015006.md): Skin · cracked · Oct 11, 2002 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STA 747 & STA 767 AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30-3 FIG.6 SHEET 4.
- [SDR CA021009024](https://openairdocs.org/sdr/CA021009024.md): Skin · cracked · Oct 7, 2002 · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > (CAN) A 4 INCH CRACK,RUNNING FORE & AFT WAS FOUND DIRECTLY ABOVE STRINGER 16L AT STATION 520. CRACK REPAIR ACCOMPLISHED AS PER 737 SRM 53-30-3.
- [SDR CA020819009](https://openairdocs.org/sdr/CA020819009.md): Dump Valve · leaking · Aug 14, 2002 · Boeing 7372Q9 · Lavatories
  > (CAN) FORWARD LAVATORY FLUID BYPASSED DUMP VALVE ASSEMBLY INTO DRAIN MAINIFOLD AND LEAKED INTO THE SERVICE PANEL AREA. AIRCRAFT WAS AT 32,000 FT AT A TEMP OF -17C, OAT, WHEN THE ICE SHED FROM THE FWD LAV SERVICING PANEL AND CONTACTED THE RT INBOARD WING AND HO
- [SDR CA020812003](https://openairdocs.org/sdr/CA020812003.md): Connector · burned · Aug 10, 2002 · Boeing 7372Q9 · APU System Wiring
  > (CAN) ON TURNAROUND, WHEN FLT CREW SELECTED APU GENERATOR ON LINE, SEVERAL C/B,S TRIPPED. GENERATOR VOLTAGE LOW UNDER LOAD,BUT DID NOT TRIP OFF BUS. FOUND BTB TERMINAL CONNECTOR BOLT BURNED & LOOSE. BTB REPLACED. CHECKED SERVICEABLE.
- [SDR DHL2002741002](https://openairdocs.org/sdr/DHL2002741002.md): Battery · discharged · Feb 1, 2002 · N741DH · Boeing 7372Q9 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED BATTERIES IN BOTH EMERGENCY LIGHTS, OPS CHECK GOOD IAW BMM CH 33-50-01.
- [SDR TSAA0133143](https://openairdocs.org/sdr/TSAA0133143.md): Light · inoperative · Oct 20, 2001 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133141](https://openairdocs.org/sdr/TSAA0133141.md): Battery Pack · discharged · Oct 20, 2001 · N804AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133140](https://openairdocs.org/sdr/TSAA0133140.md): Light · inoperative · Oct 10, 2001 · N804AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED FORWARD OVERHEAD EMERGENCY AISLE LIGHT ASSEMBLY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133108](https://openairdocs.org/sdr/TSAA0133108.md): Battery Pack · inoperative · Aug 9, 2001 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 6 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133105](https://openairdocs.org/sdr/TSAA0133105.md): Battery Pack · inoperative · Aug 3, 2001 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 3 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133103](https://openairdocs.org/sdr/TSAA0133103.md): Battery Pack · inoperative · Aug 3, 2001 · N804AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153090](https://openairdocs.org/sdr/TSAA0153090.md): Skin · cracked · Jul 23, 2001 · N804AL · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > IDENTIFIED 1.5 INCH FUSELAGE SKIN CRACK AT BS 727, S16R. REMOVED TWO PREVIOUS REPAIRS IN THE IMMEDIATE AREA, TRIM OUT DAMAGED AREA, HFEC INSPECTION COMPLETED AROUND TRIM AREA NO DEFECTS NOTED,.040 INCH INSURANCE CUT COMPLETED, VISUALLY INSPECTED AREA UNDER R
- [SDR TSAA0153063](https://openairdocs.org/sdr/TSAA0153063.md): Skin · dented · May 21, 2001 · N809AL · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > DENT AT FUSELAGE SKIN AT BS 360-BS400, STRINGER 17L. REMOVED DAMAGED AREA, HFEC INSPECTION COMPLETED NO DEFECTS NOTED AROUND CUTOUT AREA, INSTALLED 7075-T6 CREASE BEAM, INSTALLED.071 INCH FILLER 2024-T3 INSTALLED.032 INCH DOUBLER 2024-T3, INSTALLED.050 INC
- [SDR CA010515004](https://openairdocs.org/sdr/CA010515004.md): Isolation Valve · leaking · Apr 20, 2001 · Boeing 7372Q9 · Landing Gear Brake System
  > (CAN) AIRCRAFT LOST A SYSTEM HYDRAULIC FLUID UPON TAXIING TO THE TERMINAL. CREW HAD TO USE DIFFERENTIAL BRAKING TO GET TO GATE. AFTER INVESTIGATION IT WAS DETERMINED THAT THE MAIN GEAR ISOLATION VALVE P/N 65-44581-6, S/N 0575 WAS LEAKING.
- [SDR TSAA0133026](https://openairdocs.org/sdr/TSAA0133026.md): Battery Pack · discharged · Mar 3, 2001 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED FORWARD ENTRY IDENT LIGHT ASSEMBLY DUE TO BEING INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133017](https://openairdocs.org/sdr/TSAA0133017.md): Battery Pack · discharged · Feb 16, 2001 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED FORWARD SERVICE EMERGENCY EXIT IDENT AND RIGHT CENTER EXIT IDENT BATTERY PACKS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR CA010308011](https://openairdocs.org/sdr/CA010308011.md): Wire · chafed · Feb 8, 2001 · Boeing 7372Q9 · Electrical Power System Wiring
  > (CAN) WIRE W200-453-06 CHAFED THROUGH INSULATION AND WIRE. LENGTH & WIDTH OF CHAFE IS 3/8 INCH, DEPTH 1/8 INCH. APPEARS TO HAVE RUBBED AGAINST COWLING AT SOME TIME. HOWEVER, AT TIME OF DISCOVERY, IT WAS NOT APPARENT WHAT THE WIRE HAD CHAFED. THERE HAD BEEN NO
- [SDR TSAA0033240](https://openairdocs.org/sdr/TSAA0033240.md): Battery Pack · discharged · Dec 11, 2000 · N804AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 1, NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR USAASB00300](https://openairdocs.org/sdr/USAASB00300.md): Battery Pack · discharged · Oct 24, 2000 · N231US · Boeing 7372Q9 · Emergency Lighting
  > TPA - FOUND THE R2 AND L2 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE AFT CARGO BATTERY PACK. (M)
- [SDR CA001102014](https://openairdocs.org/sdr/CA001102014.md): Actuator · cracked · Sep 25, 2000 · Boeing 7372Q9 · Leading Edge Slat Actuator
  > (CAN) ON LANDING DURING GROUND SPOILER DEPLOYMENT HYDRAULIC FLUID WAS OBSERVED LEAKING FROM THE NR 5 GROUND SPOILER NR 5 ACTUATOR. OBSERVATION REVEALED THAT UNDER PRESSURE A CRACK WOULD OPEN UP IN THE CASE. SPOILER ACTUATOR WAS REPLACED. CHECKED SERVICEABLE.
- [SDR TSAA0053209](https://openairdocs.org/sdr/TSAA0053209.md): Stringer · damaged · Sep 8, 2000 · N804AL · Boeing 7372Q9 · Fuselage Main, Longeron/Stringer
  > FABRICATED AND INSTALLED STRIGNER S21R BETWEEN BS 947 TO BS 967 DUE TO RUPTURED PORTABLE WATER TANK, IAW SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 20010104AP004](https://openairdocs.org/sdr/20010104AP004.md): Relief Valve · inoperative · Sep 8, 2000 · N804AL · Boeing 7372Q9 · Cabin Pressure Control System
  > FLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUP
- [SDR TSAA0038201](https://openairdocs.org/sdr/TSAA0038201.md): Regulator · inoperative · Sep 8, 2000 · N804AL · Boeing 7372Q9 · Cabin Pressure Control System
  > FLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUP
- [SDR TSAA0033204](https://openairdocs.org/sdr/TSAA0033204.md): Battery Pack · inoperative · Sep 7, 2000 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 3 AND NR 5 FLOOR PROXIMITY BATTERY PACK DUE TO UNIT FAILS BATTERY TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053197](https://openairdocs.org/sdr/TSAA0053197.md): Frame · corroded · Aug 30, 2000 · N809AL · Boeing 7372Q9 · Fuselage Main, Frame
  > REMOVED CORROSION FROM INNER CHORD AT BS 1088 STRINGER 17 AND INSTALLED REPAIR ANGLES IAW ECO 3178. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053196](https://openairdocs.org/sdr/TSAA0053196.md): Keelbeam · corroded · Aug 24, 2000 · N809AL · Boeing 7372Q9 · Fuselage Main, Keel
  > REPAIRED FUSELAGE SECTION 46, BS 727 KEEL BEAM AREA SKIN AND DOUBLER DUE TO CORROSION. REMOVED CORROSION AND INSTALLED.063 INCH AND.050 INCH FILLER AND.063 INCH DOUBLER IAW ECO 2454. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033193](https://openairdocs.org/sdr/TSAA0033193.md): Battery Pack · inoperative · Aug 21, 2000 · N804AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR USAASB00210](https://openairdocs.org/sdr/USAASB00210.md): Valve · failed · Aug 7, 2000 · N231US · Boeing 7372Q9 · Engine Bleed Air System
  > BWI - FLT 2633 - ON CLIMB-OUT FROM BWI, THE NR 1 ENGINE BLEED TRIP OFF LIGHT ILLUMINATED (RESET WAS SUCCESSFUL) AND THE EGT WENT TO 645 DEGREES FOR 5 SECONDS. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THIS OCCURRED DURING FLAP RETRACTION AT 1,500 FEET. CREW
- [SDR TSAA0033170](https://openairdocs.org/sdr/TSAA0033170.md): Battery Pack · inoperative · Jul 8, 2000 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 2 AND NR 5 FLOOR PROXIMITY BATTERY PACK DUE TO UNIT FAILS BATTERY TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033171](https://openairdocs.org/sdr/TSAA0033171.md): Light · inoperative · Jul 8, 2000 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT ASSEMBLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033172](https://openairdocs.org/sdr/TSAA0033172.md): Light · inoperative · Jul 8, 2000 · N809AL · Boeing 7372Q9 · Emergency Lighting
  > REPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0027136](https://openairdocs.org/sdr/TSAA0027136.md): Transmitter · malfunctioned · May 17, 2000 · N804AL · Boeing 7372Q9 · Trailing Edge Flap Control System
  > FLT 91 - OGG-HNL - DURING TAKEOFF FROM OGG, THE STALL WARNING STICK SHAKER BEGAN AT ROTATION AND WAS CONTINUOUS THROUGH 1000 FEET AND INTERMITTENT AFTER THAT. RETURNED TO OGG FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITT
- [SDR TSAA0053143](https://openairdocs.org/sdr/TSAA0053143.md): Lap Joint · cracked · May 10, 2000 · N804AL · Boeing 7372Q9 · Fuselage Main, Plate/Skin
  > LOWER SKIN LAP JOINT, CRACK REPAIR AND LAP JOINT MODIFICATION COMPLETED AT BS 360-540, STRINGER 14R, STRINGER 10R, STRINGER 10L AND STRINGER 14L, BS 727-908, STRINGER 14R, 10R, STRINGER 10L AND STRINGER 14L, BS 360-908 IAW ECO 3080R1. AIRCRAFT RETURNED TO SER

Next page: https://openairdocs.org/model/boeing-737-2q9/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 = '7372Q9'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2q9/reports

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