# Service difficulty reports: Boeing 737-71B

A list on [Boeing 737-71B](https://openairdocs.org/model/boeing-737-71b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 16 · 756 reports

- [SDR SWAA2026062514979](https://openairdocs.org/sdr/SWAA2026062514979.md): Light · damaged · Jun 23, 2026 · N7852A · Boeing 73771B · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 27ABC PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R & R CABIN PHOTO LUMINESCENT STRIP PER AMM 33-51-15.
- [SDR SWAA2026061612709](https://openairdocs.org/sdr/SWAA2026061612709.md): Lamp · inoperative · Jun 16, 2026 · N7854B · Boeing 73771B · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS R2 EXTERIOR EMERGENCY EXIT LIGHT IAW AMM 33-51-01.
- [SDR SWAA2026040785726](https://openairdocs.org/sdr/SWAA2026040785726.md): Cover · out of adjust · Apr 1, 2026 · N7852A · Boeing 73771B · Emergency Lighting
  > COVER MISSING ON EMERGENCY LIGHT SWITCH NEAR AFT JUMPSEAT. SECURED COVER ON EMER LIGHT SWITCH PER SIP.
- [SDR SWAA2025111132874](https://openairdocs.org/sdr/SWAA2025111132874.md): Attach Bracket · damaged · Nov 7, 2025 · N7845A · Boeing 73771B · Fuselage Main, Attach Fittings
  > LEFT WING UPPER OTBD MLG SUPPORT BEAM ATTACH BRACKET HAD ELONGATED HOLES. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.
- [SDR SWAA2025111132736](https://openairdocs.org/sdr/SWAA2025111132736.md): Isolator Mount · cracked · Nov 7, 2025 · N7845A · Boeing 73771B · Service Doors
  > FWD SERVICE DOOR AFT UPPER SLIDE ISOLATOR MOUNT CRACKED. R & R FWD SERVICE DOOR AFT UPPER SLIDE ISOLATOR MOUNT IAW AMM 52-40-02.
- [SDR SWAA2025102024700](https://openairdocs.org/sdr/SWAA2025102024700.md): Door · cracked · Oct 16, 2025 · N7852A · Boeing 73771B · Landing Gear Doors
  > LEFT MAIN LANDING GEAR CENTER DOOR HAS CRACK. REMOVED LT MLG CENTER & INNER DOOR IAW AMM 32-13-11, OK TO CONTINUE SERVICE.
- [SDR SWAA2025090811674](https://openairdocs.org/sdr/SWAA2025090811674.md): Scuff Plate · missing · Sep 5, 2025 · N7849A · Boeing 73771B · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SCUFF PLATE HAS MISSING MATERIAL AND SHARP EDGE. R&R FWD CARGO DOOR SCUFF PLATE REF AMM 25-52-10. COMPLETED R&R OF FWD CARGO DOOR SCUFF PLATE REF AMM 53-11-02.
- [SDR SWAA2025090209827](https://openairdocs.org/sdr/SWAA2025090209827.md): Cover · missing · Aug 29, 2025 · N7849A · Boeing 73771B · Emergency Lighting
  > RIGHT SIDE OVERWING EXIT ROW; LOWER LIGHT COVER MISSING. REPLACED RH OVER-WING EXIT EMERGENCY LIGHT LENS COVER REF AMM 33-51-01.
- [SDR SWAA2025082909176](https://openairdocs.org/sdr/SWAA2025082909176.md): Lamp · inoperative · Aug 28, 2025 · N7849A · Boeing 73771B · Emergency Lighting
  > FORWARD L1 ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP, L1 EMERGENCY LIGHT IAW AMM 33-51-03 OPS CHECK GOOD.
- [SDR SWAA2025071792178](https://openairdocs.org/sdr/SWAA2025071792178.md): Bracket · loose · Jul 16, 2025 · N7852A · Boeing 73771B · Emergency Equipment
  > ENTRY GIRT BAR ATTACHMENT LOOSE. ADJUSTED GIRT BAR ATTACH BRACKET PER SIP; OPS CK GOOD.
- [SDR SWAA2025071791911](https://openairdocs.org/sdr/SWAA2025071791911.md): Retainer · detached · Jul 15, 2025 · N7849A · Boeing 73771B · Emergency Equipment
  > FWD SERVICE DOOR SLIDE COVER RETAINING CLIP FELL OFF<[01] INSTALLED CLIO AS REQ PER AMM 25-66-01
- [SDR SWAA2025052774487](https://openairdocs.org/sdr/SWAA2025052774487.md): Sleeve · missing · May 23, 2025 · N7852A · Boeing 73771B · Emergency Equipment
  > AFT LEFT GIRTBAR DISARMED ON LANDING MISSING STOPPER/ STOP SLEEVE.<[01] INSTALLED NEW GIRT BAR STOP SLEEVE PER AMM 25-66-01
- [SDR SWAA2025050666893](https://openairdocs.org/sdr/SWAA2025050666893.md): Light · inoperative · May 3, 2025 · N7854B · Boeing 73771B · Emergency Lighting
  > EMERGENCY EXIT WALL LIGHT AFT OF RH EMERGENCY DOOR IS INOP<[01] R/R EMERG EXIT WALL LIGHT ASSY AFT OF RH EMERG DOOR PER AMM 33-51-01. OPS CHECKS GOOD.
- [SDR SWAA2025043065811](https://openairdocs.org/sdr/SWAA2025043065811.md): Engine · power loss · Apr 30, 2025 · N7849A · Boeing 73771B · Engine (Turbine/Turboprop)
  > ON INITIAL TAKEOFF ROLL (LESS THAN 40 KTS) #1 ENGINE WOULD NOT INDICATE MORE THAN 70% N1 A LEFT YAW FOLLOWED TAKEOFF WAS REJECTED; NO ADNORMAL INDICATIONS NOTED<[01] T/S PER FIM 73-05 TASK 808. NO FAULTS FOUND. PERFORMED POWER PLANT POWER ASSURANCE CHECK PER
- [SDR SWAA2025042125630](https://openairdocs.org/sdr/SWAA2025042125630.md): Handle · loose · Apr 17, 2025 · N7854B · Boeing 73771B · Service Doors
  > FWD GALLEY SERVICE DOOR R1 INTERIOR HANDLE LOOSE.<[01] RE-SECURED FWD GALLEY SERVICE DOOR INTERIOR HANDLE REF AMM 20-50-11.
- [SDR SWAA2025033109875](https://openairdocs.org/sdr/SWAA2025033109875.md): Seal · cracked · Mar 27, 2025 · N7852A · Boeing 73771B · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)]R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL;[02] CHANGED RII
- [SDR SWAA2025032709877](https://openairdocs.org/sdr/SWAA2025032709877.md): Battery Pack · no test · Mar 27, 2025 · N7852A · Boeing 73771B · Emergency Lighting
  > EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1675; M1669; M1672<[01] REMOVED AND REPLACED EMERGENCY LIGHT BASE AND BATTERY AT M1674; AND BATTERIES AT M1675; M1669; M1672 PER AMM 33-51-06
- [SDR SWAA2025032408181](https://openairdocs.org/sdr/SWAA2025032408181.md): Engine · surges · Mar 20, 2025 · N7852A · Boeing 73771B · Engine (Turbine/Turboprop)
  > DURING DESCENT NR 2 ENGINE BEGAN SHAKING AND MAKING NOISES AND N1 DROPPED TO 41% N1. RAN ENGINE LIMITS /SURGE/STALL QRH AFTER SEVERAL MOMENTS, NR 2 ENGINE OPERATED NORMALLY AND OPERATED NORMALLY REMAINDER. PERFORMED FIM 71-05 TASK 805. PER STEP E.(2), PERFORME
- [SDR SWAA2025021094295](https://openairdocs.org/sdr/SWAA2025021094295.md): Lamp · inoperative · Feb 8, 2025 · N7854B · Boeing 73771B · Emergency Lighting
  > AFT R/H SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED AFT R/H SERVICE DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025013090656](https://openairdocs.org/sdr/SWAA2025013090656.md): Battery Pack · failed · Jan 29, 2025 · N7845A · Boeing 73771B · Emergency Lighting
  > AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)].
- [SDR SWAA2025012890114](https://openairdocs.org/sdr/SWAA2025012890114.md): Bushing · broken · Jan 27, 2025 · N7849A · Boeing 73771B · Emergency Equipment
  > R-1 DOOR GIRT BAR PLASTIC BUSHING BROKEN <[01]. REMOVED AND REPLACED PER AMM 25-66-01.
- [SDR SWAA2025012890115](https://openairdocs.org/sdr/SWAA2025012890115.md): Skin · delaminated · Jan 27, 2025 · N7845A · Boeing 73771B · Trailing Edge Flaps
  > L/H INBOARD MAIN FLAP DELAMINATED AT TRAILING EDGE DELAMINATION IS 22.5 LENGTH 9.5 WIDTH 3.5 INCHES FROM OUTBOARD EDGE OF LH INBOARD MAIN FLAP<[01] COMPLIED WITH EA 25-157-00209. REINSPECT DUE EVERYDAY 8 DAYS WITH PERMANENT REPAIR DUE WITHIN 131 DAYS. REF FAUL
- [SDR SWAA2024122680428](https://openairdocs.org/sdr/SWAA2024122680428.md): Light · inoperative · Dec 23, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR IAW AMM 33-51-04; OPS CHECK GOOD.
- [SDR SWAA2024120272936](https://openairdocs.org/sdr/SWAA2024120272936.md): Handle · broken · Nov 30, 2024 · N7854B · Boeing 73771B · Passenger/Crew Doors
  > AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] REPLACED ASSIT HANDLE FROM AFT LAV; AFT LAV ASSIT HANDLE NOW MISSING; OK TO CONTINUE PER MEL 25-10-01 SP1B;[02] INSTALLED AFT LAV HANDLE WHICH WAS REMOVED TO COMPLY WITH MEL 25-10-01 IAW CMM 25-42-60. MEL CLEARED.
- [SDR SWAA2024112670546](https://openairdocs.org/sdr/SWAA2024112670546.md): Isolation Mount · cracked · Nov 22, 2024 · N7854B · Boeing 73771B · Escape Slide
  > AFT ENTRY DOOR FWD SLIDE MOUNT UPPER ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT UPPER ISOLATOR IAW SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024112670547](https://openairdocs.org/sdr/SWAA2024112670547.md): Light · inoperative · Nov 22, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > L/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-01;[02] 02 - INSPECTED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2024102250556](https://openairdocs.org/sdr/SWAA2024102250556.md): Retainer · loose · Oct 19, 2024 · N7854B · Boeing 73771B · Emergency Equipment
  > CUSTOMER REQUEST MAIN ENTRY DOOR SLIDE BAR LOOSE DURING THE DOOR OPERATION (2 TIMES). 2024-573003<[01] PERFORMED AJUST GIRB BAR RETAINER CLIP IN FWD ENTRY DOOR I.AW B737-700 AMM 25-66-01-200-802 STEP 3.B(1)(F) ITEM 4)B);[02] CORRECTED STEP 1 <BR>PERFORMED AJUS
- [SDR SWAA2024100142360](https://openairdocs.org/sdr/SWAA2024100142360.md): Bulb · inoperative · Sep 27, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY EXIT LIGHT ON AFT FACE OF FWD LAV HAS 1EA INOP BULB<[01] RELAMPED AND PERFORMED GOOD TEST OF FWD ENTRY DOOR EMERGENCY EXIT LIGHT ON AFT FACE OF FWD LAV 1EA IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024100142359](https://openairdocs.org/sdr/SWAA2024100142359.md): Bulb · inoperative · Sep 27, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE SEAT ROW 18ABC HAS 1EA INOP BULB<[01] REPLACED LAMPS AND PERFORMED GOOD TEST OF EMERGENCY EXIT SIGN ON CEILING LOCATED ABOVE SEAT ROW 18ABC PER AMM 33-51-01-960-801;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024100142353](https://openairdocs.org/sdr/SWAA2024100142353.md): Light · inoperative · Sep 26, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > R/H FWD EMERGENCY ESCAPE SLIDE LIGHT INOP<[01] RELAMPED R/H FWD EMERGENCY ESCAPE SLIDE LIGHT AND PERFORMED GOOD TEST IAW AMM 33-51-04-960-801;[02] INDEPENDENT INSPECTION SELECTED IN ERROR. NO INDEPENDENT INSPECTION NEEDED.;[03] VERIFIED CORRECTIVE ACTIONS 1 AN
- [SDR SWAA2024100142354](https://openairdocs.org/sdr/SWAA2024100142354.md): Battery Pack · inoperative · Sep 26, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > EMERGENCY LIGHT IN FWD COVE CEILING PANEL INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674 AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805. EMERGENCY LIGHT IN FWD COVE CEILING PANEL NOW WORKS.;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2024100142352](https://openairdocs.org/sdr/SWAA2024100142352.md): Light · inoperative · Sep 26, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > R/H AND L/H AFT ESCAPE SLIDE LIGHTS INOP<[01] RELAMPED LEFT AFT SLIDE LIGHT AND TESTED PER AMM 33-51-04-960-801; NO DEFECTS NOTED.<BR>TROUBLESHOT RIGHT AFT SLIDE LIGHT PROBLEM TO OPEN FUSE AT M1672 PER WDM 33-51-14 AND WDM 33-51-11. REPLACED FUSE CONNECTED TO
- [SDR SWAA2024100142355](https://openairdocs.org/sdr/SWAA2024100142355.md): Lamp · inoperative · Sep 26, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > L/H OVERWING HATCH FWD AND AFT EMERGENCY LIGHT LOCATORS HAVE INOP LAMPS<[01] RELAMPED L/H OWE FWD AND AFT EMERGENCY EXIT SIGNS AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024100142356](https://openairdocs.org/sdr/SWAA2024100142356.md): Slide · out of adjust · Sep 26, 2024 · N7852A · Boeing 73771B · Escape Slide
  > AED ESCAPE SLIDE SHROUD NOT PROPPERLY INSTALLED; LOWER CATCH POINT NOT PROPERLY ENGAGED.<[01] FOUND FWD SCREW LOOSE AT AED ESCAPE SLIDE SHROUD AND TIGHTENED PER SOPM 20-50-01.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024100141851](https://openairdocs.org/sdr/SWAA2024100141851.md): Battery Pack · failed · Sep 25, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > EMERGENCY BATTERY PACK M1668 AND M1669 FAIL TEST EMERGENCY BATTERY PACK M1668 AND M1669 FAIL TEST<[01] REMOVED; REPLACED; AND PERFORMED GOOD TEST OF EMERGENCY LIGHT BATTERY PACKS; M1668 AND M1669 PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024102339868](https://openairdocs.org/sdr/SWAA2024102339868.md): Stringer · cracked · Sep 21, 2024 · N7854B · Boeing 73771B · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 15-L LOCATED BETWEEN STA 294.5 AND STA 303.9 AT FWD PASSENGER COMPARTMENT 2024-572947<[01] TOOL USED ON STEP 2 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 20
- [SDR SWAA2024100140142](https://openairdocs.org/sdr/SWAA2024100140142.md): Floor Panel · cracked · Sep 21, 2024 · N7852A · Boeing 73771B · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PNL 140DF CAP STRIP CRACKED BS 947<[01] RECEIVED NEW CAP STRIP; CAP STRIP WILL BE INSTALLED WITH FLOOR PNL ON <BR>TTG8Q00U8AF2;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024100140143](https://openairdocs.org/sdr/SWAA2024100140143.md): Floor Panel · cracked · Sep 21, 2024 · N7852A · Boeing 73771B · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PNL 140DF CAP STRIP CRACKED BETWEEN BS 887 - BS 947<[01] RECEIVED NEW CAP STRIP; CAP STRIP WILL BE INSTALL WITH FLOOR PNL ON <BR>TTG8Q00U8AF2;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024102339513](https://openairdocs.org/sdr/SWAA2024102339513.md): Floorbeam · cracked · Sep 19, 2024 · N7854B · Boeing 73771B · Fuselage Main, Floor Beam
  > AAI REPORT: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 LBL 24.75 2024-572931<[01] REPLACED PANEL BREAK FLOOR STRUCTURE AT STA 540; BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9;SRM 51-40-02-0G-0 DWG
- [SDR SWAA2024102339515](https://openairdocs.org/sdr/SWAA2024102339515.md): Floorbeam · cracked · Sep 19, 2024 · N7854B · Boeing 73771B · Fuselage Main, Floor Beam
  > AAI REPORT: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 RBL 24.75 2024-572932<[01] INSTALLED NEW PANEL BREAK AND PLATE AND FASTENERS FLOOR STRUCTURE AT STA 540; BL 0 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 DWG 14
- [SDR SWAA2024100139386](https://openairdocs.org/sdr/SWAA2024100139386.md): Light · broken · Sep 19, 2024 · N7852A · Boeing 73771B · Emergency Lighting
  > AFT ENTRY LOWER CEILING PANEL EMERGENCY EXIT LIGHT ATTACH POINTS BROKEN<[01] REMOVED AND REPLACED AFT ENTRY LOWER CEILING PANEL EMERGENCY EXIT LIGHT IAW SRM 51-40-02-0G-0;[02] CERTIFY ACTION 1;[03] REMOVED AND REPLACED AFT ENTRY LOWER CEILING PANEL EMERGENCY E
- [SDR SWAA2024102339202](https://openairdocs.org/sdr/SWAA2024102339202.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO 400 BL0 2024-572914<[01] REPLACED ANGLE LOC. FLOOR STRUCTURE BTW BS 380 UP TO 400 BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 92 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[0
- [SDR SWAA2024102339204](https://openairdocs.org/sdr/SWAA2024102339204.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO BS 400 RBL 10 2024-572916<[01] REPLACED ANGLE LOCATED BTW BS 380 UP TO BS 400 RBL 10 IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV.A<BR>SEE INDIVIDUAL SING-OFF BELLOW;[02] CERTIFIED CORRECTI
- [SDR SWAA2024102339203](https://openairdocs.org/sdr/SWAA2024102339203.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO BS 400 LBL 13 2024-572915<[01] REPLACED ANGLE AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 38 REV- SEE INDIVID
- [SDR SWAA2024102338582](https://openairdocs.org/sdr/SWAA2024102338582.md): Support Angle · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-572892<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV.?<BR>M
- [SDR SWAA2024102338579](https://openairdocs.org/sdr/SWAA2024102338579.md): Support Bracket · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 727 AT LEVEL STR 27R ON FWD PARTITION AT AFT CARGO COMPARTMENT 2024-572887<[01] REPLACED SUPPORT BRACKET LOCATED BS 727 AT LEVEL STR 27R ON FWD PARTITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-0
- [SDR SWAA2024102238577](https://openairdocs.org/sdr/SWAA2024102238577.md): Support · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572885<[01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG#146A7500; SHEET:85;
- [SDR SWAA2024102238580](https://openairdocs.org/sdr/SWAA2024102238580.md): Shield · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 787 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572888<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TE
- [SDR SWAA2024102238581](https://openairdocs.org/sdr/SWAA2024102238581.md): Angle · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572890<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-10-02
- [SDR SWAA2024102238583](https://openairdocs.org/sdr/SWAA2024102238583.md): Web · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24.75 AT AFT CARGO COMPARTMENT 2024-572893<[01] REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24.75 AT AFT CARGO COMPARTMENT I.A.W DWG 149A8100 SHEET: 1 REV: - AND B737-700 SRM 51-40-02-0G

Next page: https://openairdocs.org/model/boeing-737-71b/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 = '73771B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-71b/reports

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