# Service difficulty reports: Boeing 737-2Q8

A list on [Boeing 737-2Q8](https://openairdocs.org/model/boeing-737-2q8.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 133 reports

- [SDR 2023F00020](https://openairdocs.org/sdr/2023F00020.md): Frame · cracked · Jan 7, 2023 · N413JG · Boeing 7372Q8 · Fuselage Main, Frame
  > STA 360 FRAME BETWEEN S20R-S21R FOUND CRACK AT THE EDGE OF FASTENER HOLE (0.31" IN LENGTH)
- [SDR 2023F00019](https://openairdocs.org/sdr/2023F00019.md): Beam · corroded · Dec 23, 2022 · N413JG · Boeing 7372Q8 · Horizontal Stabilizer Structure
  > BULGES AT LH SIDE HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM AT STAB 83 (3.0" X 1.5" IN AREA) & STA 116 (0.8" X 0.4" IN AREA)
- [SDR 2023F00018](https://openairdocs.org/sdr/2023F00018.md): Spar · corroded · Dec 23, 2022 · N413JG · Boeing 7372Q8 · Horizontal Stabilizer, Spar/Rib
  > BULGES AT LEFT HORIZONTAL STABILIZER REAR SPAR CHORD AT HSS 126.
- [SDR 2023FA0000018](https://openairdocs.org/sdr/2023FA0000018.md): Beam · corroded · Dec 23, 2022 · N413JG · Boeing 7372Q8 · Horizontal Stabilizer Structure
  > BULGES AT RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM AT HSS 68, 120, 130, AND 137.5.
- [SDR 2023F00017](https://openairdocs.org/sdr/2023F00017.md): Spar · corroded · Dec 23, 2022 · N413JG · Boeing 7372Q8 · Horizontal Stabilizer, Spar/Rib
  > BULGE AT RT HORIZONTAL STABILIZER REAR SPAR HSS 136.5.
- [SDR 2023F00016](https://openairdocs.org/sdr/2023F00016.md): Skin · corroded · Dec 22, 2022 · N413JG · Boeing 7372Q8 · Wing, Plate/Skin
  > CORROSION AT LWR LT WING SKIN SURFACE INSPAR WS 583.
- [SDR KNNA200700040](https://openairdocs.org/sdr/KNNA200700040.md): Skin · cracked · Jul 20, 2007 · N413JG · Boeing 7372Q8 · Cargo/Baggage Doors
  > AFT CARGO DOOR/CRACKED SKIN NEAR OF LATCH HANDLE, ACO NR 0753101 PROVIDE INSTRUCTIONS ON REPAIRING CRACK IN AFT CARGO DOOR SKIN NEAR HANDLE, SRM 52-30-2 FIG 3.
- [SDR KNNA200700037](https://openairdocs.org/sdr/KNNA200700037.md): Skin · cracked · Jul 11, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Frame
  > SKIN IS CRACKED AT THE LOWER FWD CORNER OF THE L-2 DOOR CUT OUT. ACO NR 075397 REV 0 PROVIDES INSTRUCTIONS ON REPAIR OF L-2 DOOR CRACK SRM 53-30-3 FIGURE 46.
- [SDR KNNA200700034](https://openairdocs.org/sdr/KNNA200700034.md): Floorbeam · corroded · May 9, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Floor Beam
  > PASSENGER CABIN/CORRODED UPPER SURFACE ON FLOORBEAM BS 941.5 AND LBL-16 TO RBL-7ACO NR 075378 REV. 0 PROVIDE INSTRUCTION ON REPAIR OF FLOOR BEAM AT BS-947.5, LBL 36-RBL 12, SRM 53-10-9 FIGURE 9.
- [SDR KNNA200700031](https://openairdocs.org/sdr/KNNA200700031.md): Shear Tie · corroded · May 8, 2007 · N413JG · Boeing 7372Q8 · Fuselage Internal Mounting Structure
  > LIGHT SURFACE CORROSION AT SHEAR TIE ON BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R, ACO NR 075370 REV 1. PROVIDE INSTRUCTIONS ON REPAIR AT BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R SRM 53-10-4 FIGURE 7.
- [SDR KNNA200700035](https://openairdocs.org/sdr/KNNA200700035.md): Frame Splice · active · May 5, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Frame
  > PASSENGER CABIN/CRACKED FRAME AT BS 767 NEAR STRINGER 14R. PROVIDE INSTRUCTIONS ON REPAIR OF CRACKED FRAME AT BS 767 STR 14R, BOEING SB 737-53A-1261 PART 3 REPAIR.
- [SDR KNNA200700027](https://openairdocs.org/sdr/KNNA200700027.md): Skin · dented · May 3, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BETWEEN STR 26R TO STR 25R AT BS 420 R, ACO NR 075366, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 420 R STR-25R-26R, SRM 53-30-3.
- [SDR KNNA200700029](https://openairdocs.org/sdr/KNNA200700029.md): Skin · damaged · Apr 29, 2007 · N413JG · Boeing 7372Q8 · Fuselage Structure (General)
  > LOWER LOBE/FUSELAGE SKIN, SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BS 807 TO BS 827 AT BBL-0. FOUND CORROSION AT THE TIME FASTENER REMOVAL. ACO NR 075369 PROVIDE REPAIRS INSTRUCTIONS ON SKIN REPAIR AT BS 807-827 BBL 0, SRM 53-10-4 FIGURE 6.
- [SDR KNNA200700032](https://openairdocs.org/sdr/KNNA200700032.md): Skin · damaged · Apr 29, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > LOWER LOBE/FUSELAGE SKIN SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BSTA-777 BBL-0. FOUND CORROSION AT FASTENER REMOVAL, ACO NR 075380. PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS-777,FROM STR-27L TO STR-27R SRM 53-30-3 FIGURE 5.
- [SDR KNNA200700039](https://openairdocs.org/sdr/KNNA200700039.md): Skin · canning · Apr 26, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > OIL-CAN EFFECT ON FUSELAGE SKIN AT BS 384 BETWEEN STR-16L/17L, ACO NR 0753100 REV.0, PROVIDE INSTRUCTIONS ON REPAIR OF DAMAGE SKIN, BETWEEN BS 360L TO BS 420L SRM 53-30-3 AND BOEING MESSAGE 1-326794229-28 AND FAA 8100-9.
- [SDR KNNA200700038](https://openairdocs.org/sdr/KNNA200700038.md): Skin · dented · Apr 26, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AT BS 358/STR-17L NEAR DOOR L-1. ACO NR 075398 REV. 0, PROVIDE INSTRUCTIONS ON REPAIR OF GOUGE FWD OF BS 360 SRM 53-30-3 AND BOEING MESSAGE 1-326794229-26 AND FAA 8100-9.
- [SDR KNNA200700036](https://openairdocs.org/sdr/KNNA200700036.md): Skin · dented · Apr 26, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > UPPER LOBE/SEVERAL DENTS ON FUSELAGE SKIN FROM BS 995 TO BS1000 BETWEEN S-15L TO S-16L, NEAR DOOR L2.ACO NR 075385 REV 0. PROVIDES INSTRUCTIONS ON REPAIR OF FUSELAGE SKIN AFT OF L2 DOOR, SRM 53-30-3 FIG 46 AND FIG 48 BOEING MESSAGE 1-377247518-4 WITH FAA 8100
- [SDR KNNA200700028](https://openairdocs.org/sdr/KNNA200700028.md): Skin · canning · Apr 26, 2007 · N413JG · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT OIL CAN EFFECT ON SKIN BETWEEN STR 22R AND STR-21R. ALSO BETWEEN STA 480R AND STA 500R ACO NR 075363, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 480-500, STR 21R-22R SRM BOEING 53-30-3.
- [SDR ASAA0711423](https://openairdocs.org/sdr/ASAA0711423.md): Squat Switch · out of adjust · Jan 29, 2007 · N741AS · Boeing 7372Q8 · Landing Gear Position and Warning
  > DURING TAKEOFF CLIMB MLG HANDLE FAILED TO RETRACT TO DETENT WITHOUT USING OVERRIDE BUTTON. MAINTENANCE FOUND WEIGHT ON WHEELS SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH, OPS CHECK GOOD.
- [SDR ASAA0711387](https://openairdocs.org/sdr/ASAA0711387.md): Bulb · missing · Jan 13, 2007 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > R2 DOOR AND RT OVERWING EXIT "EXIT MARKER" LIGHTS MISSING 1 EACH LAMP. RELAMPED BOTH EMERGENCY LIGHTS AS REQUIRED.
- [SDR ASAA0711380](https://openairdocs.org/sdr/ASAA0711380.md): Arm · out of adjust · Jan 11, 2007 · N741AS · Boeing 7372Q8 · Passenger/Crew Doors
  > L1 DOOR HARD TO CLOSE. ADJUSTED STOPS AND GUIDE ARM, OPS CHECK GOOD.
- [SDR ASAA0711358](https://openairdocs.org/sdr/ASAA0711358.md): Guide Arm · out of adjust · Jan 5, 2007 · N741AS · Boeing 7372Q8 · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE IS RELUCTANT TO STAY COMPLETELY CLOSED. ADJUSTED L1 DOOR GUIDE ARM.
- [SDR ASAA0611233](https://openairdocs.org/sdr/ASAA0611233.md): Skin · cracked · Nov 26, 2006 · N741AS · Boeing 7372Q8 · Passenger/Crew Doors
  > L1 DOOR SKIN LOWER HINGE CUTOUT CONTAINED A CRACK AT THE LWR CORNER MEASURING APPROX.0350 INCHES. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 5210 01215.
- [SDR ASAA0611190](https://openairdocs.org/sdr/ASAA0611190.md): Light · inoperative · Nov 8, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > AFT CABIN BULKHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.
- [SDR ASAA0611116](https://openairdocs.org/sdr/ASAA0611116.md): Battery · discharged · Oct 20, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > SMOKE BARRIER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY.
- [SDR ASAA0611082](https://openairdocs.org/sdr/ASAA0611082.md): Charger · inoperative · Oct 18, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > AFTER RECON L2 DOOR INTERIOR EMERGENCY LIGHT INOP. REPLACED L2 DOOR EMERGENCY EXIT LIGHT CHARGER CONTROL UNIT BATTERY PACK.
- [SDR ASAA0611077](https://openairdocs.org/sdr/ASAA0611077.md): Wire · chafed · Oct 11, 2006 · N741AS · Boeing 7372Q8 · Light System Wiring
  > WHILE TROUBLESHOOTING SCHEDULED MEL 6215944 FOR LEFT O/B LANDING LIGHT POPS C/B WHEN TURNED ON. FOUND BURNT WIRING WHERE IT GOES INTO A CONDUIT OVER THE NR 1 ENG PYLON. WIRING CHAFED AGAINST CONDUIT CAUSING IT TO SHORT OUT. EVENT BASED TECHNICAL RESPONSE IN
- [SDR ASAA0610722](https://openairdocs.org/sdr/ASAA0610722.md): Battery · discharged · Jun 22, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > SMOKE BARRIER EMERGENCY EXIT LIGHT NOT WORKING PROPERLY. REPLACED BATTERY, OPS OK.
- [SDR ASAA0610646](https://openairdocs.org/sdr/ASAA0610646.md): Light · inoperative · May 25, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT ABOVE L 1 DOOR INOP. REPLACED LIGHT ASSY. OPS NORMAL.
- [SDR ASAA0610645](https://openairdocs.org/sdr/ASAA0610645.md): Battery · discharged · May 25, 2006 · N741AS · Boeing 7372Q8 · Emergency Lighting
  > FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED R 2 EXIT LIGHT BATTERY. OPS GOOD.
- [SDR ASAA0610641](https://openairdocs.org/sdr/ASAA0610641.md): Stringer · corroded · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER CORRODED. REPLACED CORRODED STRINGER WITH NEW PART PER SRM 53 10 1.
- [SDR ASAA0610639](https://openairdocs.org/sdr/ASAA0610639.md): Skin · corroded · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > FOUND FWD CARGO PIT SKIN CORRODED. REPAIRED PER SRM 53 10 3 FIG 1.
- [SDR ASAA0610638](https://openairdocs.org/sdr/ASAA0610638.md): Skin · gouged · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > FOUND SKIN GOUGED. REPAIRED IAW EA 5330 02099.
- [SDR ASAA0610637](https://openairdocs.org/sdr/ASAA0610637.md): Skin · dented · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > FOUND EXISTING REPAIRS DAMAGED (DENTED) BEYOND LIMITS. REMOVED AND REPLACED DAMAGED REPAIRS PER EA 5330 02044
- [SDR ASAA0610633](https://openairdocs.org/sdr/ASAA0610633.md): Frame · cracked · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Frame
  > FOUND FWD ENTRY FRAME CRACKED AT FASTENER HOLE. REPLACED FRAME PER SRM 53 10 1.
- [SDR ASAA0610632](https://openairdocs.org/sdr/ASAA0610632.md): Shear Tie · gouged · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Internal Mounting Structure
  > FOUND TOOLING DAMAGE TO SHEAR TIE. REPLACED SHEAR TIE PER SRM 51 30 02.
- [SDR ASAA0610631](https://openairdocs.org/sdr/ASAA0610631.md): Stringer Clip · missing · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Attach Fittings
  > FOUND FWD CARGO PIT TIE CLIP MISSING. REPLACED MISSING TIE CLIP WITH REPLACEMENT PART PER SRM 51 30 02.
- [SDR ASAA0610630](https://openairdocs.org/sdr/ASAA0610630.md): Stringer · corroded · May 24, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND FWD CARGO PIT STRINGER CORRDED. REPLACED STRINGER WITH REPAIR PARTS PER SRM 53 10 01.
- [SDR ASAA0610614](https://openairdocs.org/sdr/ASAA0610614.md): Stringer · corroded · May 19, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 22C CORRODED. REPAIRED STRINGER 22C PER SRM 53 10 3.
- [SDR ASAA0610611](https://openairdocs.org/sdr/ASAA0610611.md): Sill · corroded · May 18, 2006 · N741AS · Boeing 7372Q8 · Fuselage Miscellaneous Structure
  > FOUND R2 DOORWAY SILL CHORD IS CORRODED. REPLACED SILL CHORD PER SRM 57 30 2.
- [SDR ASAA0610613](https://openairdocs.org/sdr/ASAA0610613.md): Stringer · corroded · May 18, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 25R CORRODED. REPAIRED STRINGER PER SRM 53 10 3.
- [SDR ASAA0610612](https://openairdocs.org/sdr/ASAA0610612.md): Stringer · corroded · May 18, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 27R IS CORRODED. REPLACED STRINGER PER SRM 53 10 1 FIG 1.
- [SDR ASAA0610610](https://openairdocs.org/sdr/ASAA0610610.md): Stringer · corroded · May 18, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND FWD CARGO PIT STRINGER CORRODED. REPAIRED BY FABRICATING AND INSTALLING REPAIR PART PER SRM 53 10 1.
- [SDR ASAA0610609](https://openairdocs.org/sdr/ASAA0610609.md): Stringer Splice · corroded · May 18, 2006 · N741AS · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > FOUND FWD CARGO STRINGER SPLICE CORRODED. REPLACED WITH FABRICATED REPAIR PART IAW SRM 51 30 02 AND 53 10 01.
- [SDR ASAA0610467](https://openairdocs.org/sdr/ASAA0610467.md): Slide Raft · malfunctioned · Apr 19, 2006 · N741AS · Boeing 7372Q8 · Escape Slide
  > UPON DEPLOYMENT OF L 1 DOOR SLIDE, SLIDE INFLATED SLOWLY AND LANYARD DID NOT RELEASE. SLIDE DID NOT TOUCH FLOOR (SLIDE) BENT IN HALF. REPLACED L1 SLIDE ASSY PER AMM 25 65 31 201.
- [SDR CA040825009](https://openairdocs.org/sdr/CA040825009.md): Cap · leaking · Aug 18, 2004 · Boeing 7372Q8 · Drag Control Actuator
  > (CAN) AIRCRAFT TURN BACK DUE TO LOSS OF HYDRAULIC FLUID SYSTEN B IN FLIGHT. ON INSPECTION FOUND PLUG ON NR2 SPOILER ACTUATOR LEAKING. REPLACED PLUG P/N 66-22774-1 IAW CMM OVH 27-60-41. B SYSTEM CASE DRAIN FILTER TO B SYSTEM PRESS FILTERS CHECKED FOR CONTAMIN
- [SDR CA040423009](https://openairdocs.org/sdr/CA040423009.md): Quick Disconnect · leaking · Apr 21, 2004 · Boeing 7372Q8 · Brake
  > (CAN) AC LANDED, ON ROLL-OUT, WAS OBSERVED TO HAVE SMOKE ISSUING FROM UNDERSIDE OF AC. TOWER ADVISED CREW AND CALLED OUT AFF. RT MAIN GEAR WAS FULLY ENGULFED IN HEAVY SMOKE. SMOKE WAS BROUGHT UNDER CONTROL AND AC PASSENGERS AND CREW EVACUATED ONTO RUNWAY. MAI
- [SDR P2EA2002M009](https://openairdocs.org/sdr/P2EA2002M009.md): Thrust Reverser · cracked · Feb 17, 2002 · N121NJ · Boeing 7372Q8 · Engine Thrust Reverser
  > ON WALK-AROUND FOUND THE NR 2 ENGINE THRUST REVERSER WITH CRACK ON THE RIGHT HAND SIDE. REPLACED THE NR 2 ENGINE THRUST REVERSER IAW MM 78-32-10, LEAK CHECK AND OPS CHECK NORMAL.
- [SDR P2EA2002M002](https://openairdocs.org/sdr/P2EA2002M002.md): Bushing · worn · Jan 10, 2002 · N121NJ · Boeing 7372Q8 · Trailing Edge Flap Actuator
  > RIGHT HAND TRAILING EDGE FLAP FLUTTERS VISIBLY AT FLAPS 5 ABOVE 200 KTS. OK AT 190 KTS AND AT ALL OTHER FLAP SETTINGS. INSPECTED AND FOUND THE NR 7 FLAP JACKSCREW GEAR BOX END UNIVERSAL JOINT BUSHINGS WORN. OVERHAULED THE NR 7 FLAP JACKSCREW GEAR BOX END UN
- [SDR P2EA2001M0018](https://openairdocs.org/sdr/P2EA2001M0018.md): Light · loose · Dec 23, 2001 · N121NJ · Boeing 7372Q8 · Emergency Lighting
  > DURING TAXI EMERGENCY EXIT LIGHT CENTER OF AIRCRAFT ON RIGHT LOOSE. RESECURED IAW MM 33-20. OPERATIONAL CHECK NORMAL.

Next page: https://openairdocs.org/model/boeing-737-2q8/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 = '7372Q8'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2q8/reports

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