# Service difficulty reports: Boeing 737-8FH

A list on [Boeing 737-8FH](https://openairdocs.org/model/boeing-737-8fh.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 171 reports

- [SDR SCNA20260925408](https://openairdocs.org/sdr/SCNA20260925408.md): Pin · damaged · Sep 24, 2026 · N821SY · Boeing 7378FH · Emergency Exits
  > DAMAGED PIN OF LATCH BLOCK OF ESCAPE SLIDE R2 DOOR. OPEN
- [SDR SCNA20260824370](https://openairdocs.org/sdr/SCNA20260824370.md): Hook · loose · Aug 22, 2026 · N821SY · Boeing 7378FH · Emergency Equipment
  > L1 DOOR SLIDE COVER - GIRT BAR "J" JOOK LOOSE. NEEDS REPAIR AND INSTALLATION. INSTALLED "J" HOOK REF 51-40-02. INSTALLED DOOR SLIDE REF 25-66-01. OK FOR SERVICE
- [SDR SCNA20260916400](https://openairdocs.org/sdr/SCNA20260916400.md): Engine · vibration · Aug 18, 2026 · N820SY · Boeing 7378FH · Engine (Turbine/Turboprop)
  > NUMBER 1 ENGINE VIBRATION AT 3.9 IN CLIMB AND 3.3 DURING CRUISE. PERFORMED VIBRATION SURVEY TEST 7 IAW AMM 71-00-00-00-700-814-F00, HIGH VIBRATION OF 3.1, PERFORMED TEST 14B AVM FAN BALANCE TRIM, REPEAT VIBRATION SURVEY TEST 7, HIGH VIBRATION OF.5 AT T/O POW
- [SDR SCNA20260803335](https://openairdocs.org/sdr/SCNA20260803335.md): Light · damaged · Aug 1, 2026 · N820SY · Boeing 7378FH · Emergency Lighting
  > DURING INSPECTION SELF-ILLIMINATING FLOOR PATH MARKING WERE FOUND SEVERAL DAMAGE - - (WORK IN PROGRESS)
- [SDR SCNA20260722322](https://openairdocs.org/sdr/SCNA20260722322.md): Slide · unraveled · Jul 22, 2026 · N821SY · Boeing 7378FH · Escape Slide
  > R1 DOOR SLIDE STARTING TO COME UNRAPPED AT LOWER FLAPPER. REMOVED RE-PACKED AND REINSTALLED R1 DOOR SLIDE IAW AMM25-66-01, SLIDE OK FOR SERVICE.
- [SDR SCNA20260814361](https://openairdocs.org/sdr/SCNA20260814361.md): Frame · cracked · Jul 20, 2026 · N820SY · Boeing 7378FH · Fuselage Main, Frame
  > INITIAL INSPECTION: CRACK ON FRAME STA 360 BTW STGR 7R/8R AT PASSENGER CABIN - -(WORK IN PROGRESS)
- [SDR SCNA20260814362](https://openairdocs.org/sdr/SCNA20260814362.md): Skin · damaged · Jul 16, 2026 · N820SY · Boeing 7378FH · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/500H AND STGR S-25L/ S-24L - - ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/-500H AND STGR S-25L/ S-24L WAS REPAIRED PER ETI-737-26-071 REV. 2, MM4-SCA-26-0024
- [SDR SCNA20260720316](https://openairdocs.org/sdr/SCNA20260720316.md): Fastener · loose · Jul 16, 2026 · N820SY · Boeing 7378FH · Emergency Equipment
  > LOOSE FASTENER ON LATCH BLOCK ASSY OF ESCAPE SLIDE PACK AT FWD PASSENGER ENTRY DOOR. OPEN
- [SDR ASAA2026061266770](https://openairdocs.org/sdr/ASAA2026061266770.md): Door · no discrepancy · Jun 12, 2026 · N549AS · Boeing 7378FH · Passenger/Crew Doors
  > FA REPORTS L1 DOOR DIFFICULT TO CLOSE& LATCH. ABNORMAL WHISTLING NOTED FROM TAKEOFF TO APPROXIMATLY 10,000. GROUNDED - YES. INSPECTED SEAL AND CLEANED REF 52-11-00 AMM, NO DEFECTS NOTED. ACCOMPLISHED PRESSURIZATION CHECK. NO SQUEAL HEARD. NO HISTORY WITHIN 30
- [SDR ASAA2026042865763](https://openairdocs.org/sdr/ASAA2026042865763.md): Lamp · inoperative · Apr 28, 2026 · N549AS · Boeing 7378FH · Emergency Lighting
  > L1 SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED L1 SLIDE EMERGENCY LIGHT REF AMM 33-51-04.
- [SDR SCNA20260305109](https://openairdocs.org/sdr/SCNA20260305109.md): Dispenser · damaged · Mar 2, 2026 · N821SY · Boeing 7378FH · Cabin Equipment/Furnishings
  > R2 SOAP DISPENSER IS SHARP & RUSTED. REPLACED SOAP DISPENSOR REF CMM 25-48-12. OPS CHK GOOD.
- [SDR SCNA20260210064S](https://openairdocs.org/sdr/SCNA20260210064S.md): Strip · not reported · Feb 7, 2026 · N820SY · Boeing 7378FH · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED THE AFT GALLEY FLOOR TO CARPET TRANSITION STRIP IAW AMM 25-27-21 OPS CHECK GOOD THIS CLEARS MEL 25-10N MDDR# 136733
- [SDR SCNA20260210064](https://openairdocs.org/sdr/SCNA20260210064.md): Carpet · loose · Feb 7, 2026 · N820SY · Boeing 7378FH · Passenger Compartment Equipment
  > AFT GALLEY CARPET TO FLOOR TRANSITION TRIPPING HAZARD. OPEN
- [SDR SCNA20260108016](https://openairdocs.org/sdr/SCNA20260108016.md): Light · inoperative · Jan 7, 2026 · N821SY · Boeing 7378FH · Emergency Lighting
  > ABOVE AISLE EMERGENCY LIGHTS INOP. AT ROW 5, 10, AND 14DEF. REMOVED AND REPLACED BATTERY PACK AT ROW 11 IAW AMM 33-51-06 OPS CHECK GOOD. OK FOR SERVICE.
- [SDR SCNA20260106009](https://openairdocs.org/sdr/SCNA20260106009.md): Light · inoperative · Jan 3, 2026 · N821SY · Boeing 7378FH · Emergency Lighting
  > ABOVE AISLE EMERGENCY LIGHTS INOP. AT ROW 5, 10, AND 14DEF. ( INTERIOR EMERGENCY EXIT LIGHTING SYSTEM; EMERGENCY AISLE LIGHTS) REMOVED AND REPLACED BATTERY PACK AT ROW 11 IAW AMM 33-51-06 OPS CHECK GOOD. OK FOR SERVICE THIS CLEARS MEL.
- [SDR SCNA20260102002](https://openairdocs.org/sdr/SCNA20260102002.md): Girt Bar · unsecure · Jan 1, 2026 · N820SY · Boeing 7378FH · Emergency Equipment
  > R1 GIRT BAR NOT IN PLACE TIGHTLY. INSPECTED FITMENT ON R1 SLIDE GIRT BAR. NO DEFECTS NOTED. GIRT BAR FITMENT IN SPEC. IAW AMM 25-66-00
- [SDR ASAA2025122363358](https://openairdocs.org/sdr/ASAA2025122363358.md): Power Supply · inoperative · Dec 23, 2025 · N549AS · Boeing 7378FH · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1672 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1672, OPS CHECK GOOD REF B737 AMM 33-51-06.
- [SDR ASAA2025122363357](https://openairdocs.org/sdr/ASAA2025122363357.md): Power Supply · inoperative · Dec 23, 2025 · N549AS · Boeing 7378FH · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M2335 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M2335, OPS CHECK GOOD REF B737 AMM 33-51-06.
- [SDR ASAA2025122363356](https://openairdocs.org/sdr/ASAA2025122363356.md): Power Supply · inoperative · Dec 23, 2025 · N549AS · Boeing 7378FH · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1675 ARE INOPERATIVE. GROUNDED - YES. REMOVED, REPLACED AND OPS TEST PERFORMED SUCCESSFULLY OF THE M1675 S/N 10929 POWER SUPPLY EMERGENCY LIGHTS IAW AMM 33-51-06-960-806.
- [SDR ASAA2025122363355](https://openairdocs.org/sdr/ASAA2025122363355.md): Power Supply · inoperative · Dec 23, 2025 · N549AS · Boeing 7378FH · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1670 ARE INOP. GROUNDED - YES. REMOVED & REPLACED POWER SUPPLY M1670 S/N 27170, OPS CHECK GOOD. REF B737 AMM 33-51-06.
- [SDR ASAA2025121363119](https://openairdocs.org/sdr/ASAA2025121363119.md): Floor Panel · damaged · Dec 13, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-23 REQUIRES REPAIRED 4 EACH HOLES NEED TO PLUGGED. GROUNDED - YES. ACCOMPLSIHED PERMANENT REPAIR TO AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-23 IAW ASA B737-800 SRM 53-70-50-2R-0, 53-00-50-2R-6, & 53-00-50-2R-0.
- [SDR ASAA2025121363118](https://openairdocs.org/sdr/ASAA2025121363118.md): Floor Panel · damaged · Dec 13, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-28 (STA 986 SIDE) REQUIRES REPAIRED (PLUG OF DELETE HOLES) MARKED WITH TAPE. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-28 IAW ASA B737-800 SRM 53-70-50-2R-0, 53-00-5
- [SDR ASAA2025113063086](https://openairdocs.org/sdr/ASAA2025113063086.md): Support · corroded · Nov 30, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA STA 986 AT RBL 32 HAS A WALL SUPPORT (PN: 147A5710) THAT HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 ORIGINAL.050" REMAINING.030" REMOVED AND REPLACED WALL SUP
- [SDR ASAA2025113063085](https://openairdocs.org/sdr/ASAA2025113063085.md): Support · corroded · Nov 30, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA BS 986, LBL 32 HAS A WALL SUPPORT (PN:147A5710) THAT HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND OUT OF LIMITS ORI. MAT.050, MAT. REMAINING.032 IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR WALL SUPPORT STA 98
- [SDR ASAA2025113063084](https://openairdocs.org/sdr/ASAA2025113063084.md): Floor Support · corroded · Nov 30, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA (SEC. 47) STA 947 TO STA 967 FLOOR SUPPORT AT RBL 16 HAS CORROSION ON THE UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT AT STA 951 RBL 16-RBL 24, LOST.018" OF MATERIAL. FOUND BEYOND LIMITS IAW SRM 53-70-51-1A-1, REM
- [SDR ASAA2025113063083](https://openairdocs.org/sdr/ASAA2025113063083.md): Floor Support · corroded · Nov 30, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT, BS 967 - 986, LBL 14 HAD AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, ORIGINAL.071" REMAINING.051" REMOVED.020". REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 140A9
- [SDR ASAA2025112663082](https://openairdocs.org/sdr/ASAA2025112663082.md): Floor Support · corroded · Nov 26, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FLOOR SUPPOR BS 947-967, LBL 24 HAD SEVERAL AERAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON THE FLOOR SUPPORT BS 947-967, LBL 24, LOST.035" OF MATERIAL FOUND BEYOND LIMITS IAW SRM 53-70-51-1A-1, R & R THE FLOOR SUPPORT, PO# 1138081.2 IAW SRM 51-40
- [SDR ASAA2025112663081](https://openairdocs.org/sdr/ASAA2025112663081.md): Floor Support · corroded · Nov 26, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT BS 947-967 RBL 24 HAS SEVERAL AERAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT AT BS 947-967, RBL 24, LOST.030" OF MATERIAL FOUND BEYOND LIMITS IAW SRM 53-70-51-1A-1, REMOVED AND REPLACED INTERCOSTAL. PO 1138081.1 IAW S
- [SDR ASAA2025112162749](https://openairdocs.org/sdr/ASAA2025112162749.md): Baffle · cracked · Nov 21, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FWD CARGO PIT LT BAFFLE CRACKED BS 500 - 500A. GROUNDED - YES. REMOVED BAFFLE AT FWD CARGO BS 500-500A LT, RECEIVED BAFFLEP/N: 143A7510-17, P.O.# 1137749.1, LOCATD, DRILLED AND INSTALLED IAW DWG 143A7505, ID 0014, REV A. AND SRM 51-40-02.
- [SDR ASAA2025112062772](https://openairdocs.org/sdr/ASAA2025112062772.md): Floor Panel · delaminated · Nov 20, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL HAS COMPOSITE DAMAGE. GROUNDED - YES. EVALUATED PANEL FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS, REQUIRES FABRICATION OF NEW PANEL IAW SRM 53-00-50-1A-1, FABRIACTED FLOOR PANEL IAW SRM 53-00-50-2R-0, IPC 53-21-00-24A, DWG 143A5810, REV-, & PL143A5
- [SDR ASAA2025112062771](https://openairdocs.org/sdr/ASAA2025112062771.md): Floor Panel · damaged · Nov 20, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 143A5810-90, REV-.
- [SDR ASAA2025112062770](https://openairdocs.org/sdr/ASAA2025112062770.md): Floor Panel · damaged · Nov 20, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 143A5810-43, REV:-.
- [SDR ASAA2025112062769](https://openairdocs.org/sdr/ASAA2025112062769.md): Floor Panel · delaminated · Nov 20, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED NEW FLOOR PANEL IAW DWG 146A5810 SH 31 REV B, AND SRM 53-00-50-2R-0.
- [SDR ASAA2025112062768](https://openairdocs.org/sdr/ASAA2025112062768.md): Floor Panel · delaminated · Nov 20, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL 146A5810-71 IS DELAMINATED. GROUNDED - YES. FABRICATED NEW FLOOR PANEL IAW DWG 146A5810 SH 71 REV-, AND SRM 53-00-50-2R-0.
- [SDR ASAA2025111562559](https://openairdocs.org/sdr/ASAA2025111562559.md): Baffle · corroded · Nov 15, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT CARGO, RIGHT INTERCOSTAL BAFFLE HAS CORRODED ON THE TOP SURFACE, BS 747 - 767, S25 - S26R. GROUNDED - YES. EVALUATED BAFFLE AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN. REMOVED DAMAGED BAFFLE, LOCATED AND DRILLED NEW BAFFLE. INSTALLED NEW BAFFLE I
- [SDR ASAA2025111462748](https://openairdocs.org/sdr/ASAA2025111462748.md): Bracket · corroded · Nov 14, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT, FORWARD LOWER MAIN SILL, BRACKET ASSY HAS CORRODED IN RIGHT SIDE BS 787 - 794.37, S25R. GROUNDED - YES. EVALUATED AFT CARGO FWD LOWER MAIN SILL BRACKET ASSY. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN. REMOVED FWD LOWER MAIN SILL
- [SDR ASAA2025111163359](https://openairdocs.org/sdr/ASAA2025111163359.md): Skate Angle · cracked · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACK AT BS 661.95 LBL+7. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE IAW SRM 57-10-10-2R-5 AT BS 661.95 LBL 7.
- [SDR ASAA2025111163354](https://openairdocs.org/sdr/ASAA2025111163354.md): Angle · cracked · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACK AT BS 661.95 RBL+9. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE AT BS 661.95 RBL 9 IAW B737-800 SRM 57-10-10-2R-5 REMOVED AND REINSTALLED RT W/W EMDP IAW 29-11-21, ACCOMPLISHED
- [SDR ASAA2025111163080](https://openairdocs.org/sdr/ASAA2025111163080.md): Floorbeam · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Main, Floor Beam
  > AFT WET AREAS BS 986.5 TEE CAP APPROX. BETWEEN RBL 24 TO RBL 58 HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, FIG 104. ORIGINAL.150" LOSS OF.010" REMAINING.140". ACCOMPLISHED FULL TEE CAP R
- [SDR ASAA2025111163079](https://openairdocs.org/sdr/ASAA2025111163079.md): Floorbeam · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Main, Floor Beam
  > AFT WET AREA STA 947.5 TEE CAP APPROX. BETWEEN LBL 24 TO RBL 24 HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1 ORIGINAL.180" REMAINING.124" LOSS OF.056" ACCOMPLISHED FULL TEE CAP REPAIR AT 947 I
- [SDR ASAA2025111163078](https://openairdocs.org/sdr/ASAA2025111163078.md): Intercostal · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > RIGHT AFT INTERCOSTAL AT BS 947.5 APPROX, RBL 51 HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON INTERCOSTAL AT BS. 947 RBL 51, LOST.045" OF MATERIAL, FOUND BEYOND LIMITS IAW SRM 53-70-51-1A-1, R & R INTERCOSTAL PO 1137621.1 IAW SRM 5
- [SDR ASAA2025111163077](https://openairdocs.org/sdr/ASAA2025111163077.md): Intercostal · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > LEFT AFT INTERCOSTAL AT BS 947.5, APPROX LBL 51 HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON INTERCOSTAL AT BS 947-967 LBL 51, LOST.035" OF MATERIAL, FOUND BEYOND LIMITS IAW SRM 53-70-51-1A-1, R & R THE INTERCOSTAL. PO 1137621.2 IA
- [SDR ASAA2025111162747](https://openairdocs.org/sdr/ASAA2025111162747.md): Transition Panel · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT CARGO PIT RT TRANSITION PANEL BS 727 - 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS.040, REMOVED.040, REMAINING.000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED TRANSITION PANEL, FABRICATED NEW REPAIR USING BAC14
- [SDR ASAA2025111162745](https://openairdocs.org/sdr/ASAA2025111162745.md): Transition Panel · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FWD CARGO PIT LT TRANSITION PANEL BS 500 - 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS.040, REMOVED.040, REMAINING.000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGE TRANSITION PANEL, FABRICATED NEW REPAIR PART
- [SDR ASAA2025111162583](https://openairdocs.org/sdr/ASAA2025111162583.md): Web · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Main, Plate/Skin
  > AFT CARGO PIT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. EVALUATED AFT CARGO THRESHOLD WEB, ORIGINAL THICKNESS.045, REMOVED.024, REMAINING.021, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED DAMAGED THRESHOLD WEB IAW SRM 51-40-02 LOCATED AND DRIL
- [SDR ASAA2025111162562](https://openairdocs.org/sdr/ASAA2025111162562.md): Transition Panel · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > AFT CARGO PIT LT TRANSITION PANEL BS 727 - 847 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL 0.040, REMOVED 0.040, REMANINING 0.000, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION PANEL, FABRICATED NEW REPAIR
- [SDR ASAA2025111162561](https://openairdocs.org/sdr/ASAA2025111162561.md): Support · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FWD CARGO PIT, AFT BULKHEAD SUPPORT LOWER RAIL STA 500I HAS CORROSION. GROUNDED - YES. EVALUATED ORIG THICK=.071", REMOVED.071, REMAINING.000 100% MAT LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1. REMOVED DAMAGED RAIL, LOCATED & DRILLED NEW RAIL INS
- [SDR ASAA2025111162560](https://openairdocs.org/sdr/ASAA2025111162560.md): Transition Panel · corroded · Nov 11, 2025 · N549AS · Boeing 7378FH · Fuselage Miscellaneous Structure
  > FWD CARGO PIT RT TRANSITION PANEL STA 500A - STA 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS IS.040 REMOVED.040, REMAINING THICKNESS.000 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOST. IAW SRM 53-00-53-1A-2. REMOVED DAMAGE
- [SDR ASAA2025111063087](https://openairdocs.org/sdr/ASAA2025111063087.md): Floor Panel · damaged · Nov 10, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL 147A5810-186 HAS DAMAGED AND MISSING INSERTS. GROUNDED - YES. FABRICATED NEW FLOOR PANEL 147A5810-186 IAW B737-800 SRM 53-00-50-2R-0 AND DRAWING 1475810 REV.BT.
- [SDR ASAA2025111062773](https://openairdocs.org/sdr/ASAA2025111062773.md): Floor Panel · damaged · Nov 10, 2025 · N549AS · Boeing 7378FH · Fuselage Floor Panel
  > FLOOR PANEL HAS DAMAGED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 20EA DAMAGED INSERTS ON FLOOR PANEL IAW SRM 53-00-50-2R-0.

Next page: https://openairdocs.org/model/boeing-737-8fh/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 = '7378FH'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-8fh/reports

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