# Service difficulty reports: JASC 5310

A list on [JASC 5310](https://openairdocs.org/jasc/5310.md).

Reports filed under 5310 · Fuselage Main, Structure, newest first.

Page 1 of 769 · 38,419 reports

- [SDR FDEA202610211637](https://openairdocs.org/sdr/FDEA202610211637.md): Door Frame · cracked · Oct 21, 2026 · N745FD · Airbus A300B4622R
  > LEFT AFT PAX DOOR FRAME AT FR 73A BTWN STR 24 & 25L FOUND ONE CRACK AROUND THE RIVET HEAD OF THE SEAL RETAINER RUNOUT HOLE.
- [SDR DALA2026102205812](https://openairdocs.org/sdr/DALA2026102205812.md): Pressure Deck · cracked · Oct 20, 2026 · N3764D · Boeing 737832
  > CRACKS ON PRESSURE DECK WEB BOTH FACES STA 633 BTW LBL40-45 VIEW LH MLG WHEEL WELL. PRESSURE DECK WEB BOTH FACES STA 633 BTW LBL40-45 VIEW FROM WINGBOX AND LH MLG WHELL WELL PER B737-800 SRM 57-10-10-2R REPAIR 3, ALTERNATIVE 2 AND B737-800 SRM 57-10- 10-2R RE
- [SDR CALA2026102220530](https://openairdocs.org/sdr/CALA2026102220530.md): Plate · corroded · Oct 20, 2026 · N438UA · Airbus A320232
  > AFT CARGO BAY, AFT LAV EXHAUST VENT BETWEEN FR 69 & FR 70, STR 30R - 33R HAD CORROSION ON LOWER, INBD SIDE AT CONTACT POINT OF VENT OUTLET & AIRFRAME. R & R THE PLATE, FR 69-70 S30-33R IAW SRM 53-41-00-210 -030-C1, SRM 53-41-11-283-065, & SRM 51-72-11-911-001
- [SDR CALA2026102220524](https://openairdocs.org/sdr/CALA2026102220524.md): Crossbeam · cracked · Oct 20, 2026 · N17529 · Boeing 7379
  > BS 540, BL0 CROSSBEAM CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A5240 REV-.
- [SDR AALA202610204442](https://openairdocs.org/sdr/AALA202610204442.md): Crossbeam · cracked · Oct 20, 2026 · N961NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: STA 537 BRAKE: IS CRACKED LBL 0 TO LBL 24 AND WL0 APPROX. INSTALLED NEW BRAKE ANGLE IAW AARD 51-00-05-1.
- [SDR AALA202610200397](https://openairdocs.org/sdr/AALA202610200397.md): Crossbeam · cracked · Oct 20, 2026 · N961NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: STA 537 BRAKE ANGLE CRACKED RBL 0 TO RBL RBL24 AND WL0 APPROX. INSTALLED NEW BRAKE ANGLE IAW AARD 51-00-05-1.
- [SDR DALA2026102105793](https://openairdocs.org/sdr/DALA2026102105793.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10
  > CORROSION AT FASTENER HOLE 12IN FWD FROM AFT CARGO DOOR AFT FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319. (LP# 1874278; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102105792](https://openairdocs.org/sdr/DALA2026102105792.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10
  > CORROSION AT FASTENER HOLE 12IN AFT FROM AFT CARGO DOOR FWD FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319. (LP# 1874275; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102105791](https://openairdocs.org/sdr/DALA2026102105791.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10
  > CORROSION AT FASTENER HOLE 7IN AFT FROM AFT CARGO DOOR FWD FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319 (LP# 1874271; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102105790](https://openairdocs.org/sdr/DALA2026102105790.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10
  > CORROSION AT FASTENER HOLE 7IN FWD FROM AFT CARGO DOOR AFT FRAME. C/W ER/A 637319-14 REV ORIGINAL ASSOCIATED ER/A 14-637319 A. (LP# 1874267; AIRCRAFT WAS GROUNDED)
- [SDR REXA2026102001948](https://openairdocs.org/sdr/REXA2026102001948.md): Window Post · cracked · Oct 19, 2026 · N909XJ · Cndair CL6002D24
  > RT WINDOW SUPPORT STRAP OF THE WINDOW POST FOUND CRACKED. REPLACED RT WINDOW STRAP SUPPORT POST.
- [SDR MASA20261022233](https://openairdocs.org/sdr/MASA20261022233.md): Seal Rest · corroded · Oct 18, 2026 · N83329 · Emb ERJ170200LR
  > DURING HEAVY CHECK INSPECTIONS ON FWD CARGO DOOR CUTOUT.'LOWER MIDDLE SEAL REST CORRODED REMOVED AND REPLACED IAW SRM 51-41-01 NRC #4502703-1000-0023 REV. 45 DATED MAY-28-2021
- [SDR AALA202610218811](https://openairdocs.org/sdr/AALA202610218811.md): Vertical Support · damaged · Oct 17, 2026 · N8001N · Airbus A319115
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL MEMEBER DAMAGED AT FR24A, BL Y765. MAINTENANCE FABRICATED AND REPLACED ERTICAL MEMEBER AT FR24A, BL Y765 IAW EA 379960.
- [SDR AALA202610214183](https://openairdocs.org/sdr/AALA202610214183.md): Vertical Support · damaged · Oct 17, 2026 · N8001N · Airbus A319115
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL MEMEBER DAMAGED AT FR24A, BL Y-765. MAINTENANCE FABRICATED AND REPLACED ERTICAL MEMEBER AT FR24A, BL Y765 IAW EA 379960.
- [SDR CALA2026101920465](https://openairdocs.org/sdr/CALA2026101920465.md): Strap · cracked · Oct 15, 2026 · N23708 · Boeing 737724
  > LEFT BS 639 STUB BEAM STRAPS, AFT LOWER HOLE HAD A CRACK SIGNAL REMOVED LH STUB BEAM STRAPS DAMAGED, FABRICATED, LOCATED, DRILLED, APPLIED PRIMER AND INSTALLED NEW STUB BEAM STRAPS IAW B737-700 SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AMM 51-21-72-370-804, AMM 2
- [SDR CALA2026101920463](https://openairdocs.org/sdr/CALA2026101920463.md): Strap · cracked · Oct 15, 2026 · N23708 · Boeing 737724
  > RIGHT BS 639 STUB BEAM STRAPS, AFT LOWER HOLE HAD A CRACK SIGNAL. REMOVED RT STUB BEAM STRAPS, FABRICATED, LOCATED, DRILLED, APPLIED PRIMER AND INSTALLED NEW STUB BEAM STRAPS IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AMM 51-21-72-370-804, AMM 20-50-11-910-
- [SDR DALA2026101605697](https://openairdocs.org/sdr/DALA2026101605697.md): Door Frame · damaged · Oct 15, 2026 · N981AT · Boeing 717200
  > FOUND BENTS AND CRACKS ON AFT EDGE OF AFT CARGO DOOR CUTOUT AT Y=984 APPROX. BTW L-24R AND L-26R, REPAIRED AFT EDGE OF AFT CARGO DOOR CUTOUT PER SRM 53-20-15-2R. (1867765) (AIRCRAFT GROUNDED).
- [SDR WX0A2026101432975](https://openairdocs.org/sdr/WX0A2026101432975.md): Plate · corroded · Oct 13, 2026 · N261NV · Airbus A320214
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0092: 404-11 FWD CARGO COMPARTMENT FIXED PARTITION, PLATE AT FR34 BTW STR 35R -38R FOUND CORRODED, FWD CARGO COMPARTMENT FIXED PARTITION, PLATE AT FR34 BTW STGR35RH-STGR38RH WAS REP
- [SDR SWAA2026101243286](https://openairdocs.org/sdr/SWAA2026101243286.md): Float Valve · dirty · Oct 12, 2026 · N8314L · Boeing 7378H4
  > FOUL ODOR COMNG FROM FWD ENTRY DOOR DRAINS. REMOVED CLEANED AND REINSTALLED FWD SILL DRAIN FLOAT VALVE IAW AMM 38-31-06. LEAK CHECKS GOOD ODOR WENT AWAY
- [SDR YENA2026101500976](https://openairdocs.org/sdr/YENA2026101500976.md): Pressure Deck · cracked · Oct 11, 2026 · N558JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450766. CRACK INDICATION FOUND ON FASTENER HOLE #4 OF FR 36 PRESSURE DECK MEMBRANE LOCATED AT Y1292. CRACK DIRECTION 10 O'CLOCK LOOKING AFT. CRACK D= 0.163 INCHES.; "(RESOLVED ON W/O: 1486589 TASKC
- [SDR YENA2026101500975](https://openairdocs.org/sdr/YENA2026101500975.md): Pressure Deck · cracked · Oct 11, 2026 · N558JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450764. CRACK INDICATION FOUND ON FASTENER HOLE #7 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT Y1292. CRACK DIRECTION 11 O'CLOCK LOOKING AFT. CRACK D= 0.140 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCA
- [SDR YENA2026101500974](https://openairdocs.org/sdr/YENA2026101500974.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450763. CRACK INDICATION FOUND ON FASTENER HOLE #5 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 12 O'CLOCK LOOKING AFT. CRACK D = 0.172 INCHES.; "(RESOLVED ON W/O: 1486589 TASK
- [SDR YENA2026101500973](https://openairdocs.org/sdr/YENA2026101500973.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450762. CRACK INDICATION FOUND ON FASTENER HOLE #6 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 1 O'CLOCK LOOKING AFT. CRACK D= 0.145 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCA
- [SDR YENA2026101500972](https://openairdocs.org/sdr/YENA2026101500972.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450761. CRACK INDICATION FOUND ON FASTENER HOLE #7 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 6 O'CLOCK LOOKING AFT. CRACK D= 0.141 INCHES;"(RESOLVED ON W/O: 1486589 TASKCARD
- [SDR YENA2026101500957](https://openairdocs.org/sdr/YENA2026101500957.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, EA A26-816-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 LHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500952](https://openairdocs.org/sdr/YENA2026101500952.md): Pressure Panel · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, EA 26-817-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR JR2R20261011776](https://openairdocs.org/sdr/JR2R20261011776.md): Beam · corroded · Oct 11, 2026 · N88359 · Emb ERJ170200LR
  > AFT WET AREA LONG BEAM BETWEEN SHEAR PANEL ART RBL10 FR87 CORRODED. REPAIRED
- [SDR JR2R20261011763](https://openairdocs.org/sdr/JR2R20261011763.md): Sill Drain · corroded · Oct 11, 2026 · N88359 · Emb ERJ170200LR
  > AFT WET AREA RH MOP SILL RBL40 BETWEEN FR88 - FR90 CORRODED. REPLACED
- [SDR WX0A2026102132982](https://openairdocs.org/sdr/WX0A2026102132982.md): Post · damaged · Oct 10, 2026 · N261NV · Airbus A320214
  > (MAJOR REPAIR) (AIRCRAFT NOT GROUNDED) NRC 1000-0023: (274-11) AT FR24A, FWD CARGO BLKH POST AT Y254, VERTICAL MEMBER UPPER ATTACHMENT SECTION FOUND DAMAGED / AT FR24A, FWD CARGO BLKH POST AT Y254, VERTICAL MEMBER UPPER ATTACHMENT SECTION, PERMANENTLY REPAIRED
- [SDR UIEA2026100900972](https://openairdocs.org/sdr/UIEA2026100900972.md): Failsafe · damaged · Oct 10, 2026 · N649GT · Boeing 767375
  > DETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DEFECT SIGNAL LOCATION: FAILSAFE STRAP (RH)(<P>REMOVED PLATE ASSY OF R/H MAIN L/G W/W LONGN AND L/G BE
- [SDR UIEA2026100900974](https://openairdocs.org/sdr/UIEA2026100900974.md): Tee Fitting · cracked · Oct 10, 2026 · N649GT · Boeing 767375
  > DURING EO 6753A070 PART 4 (SB 767-53A0100 R3 / AD 2012-09-04 TERMINATING ACTION) AT STA 955 R/H, CRACKS WERE FOUND AT THE 10 O'CLOCK (0.5€?) AND 4 O'CLOCK (NOT MEASURABLE) POSITIONS FROM THE LOWEST FAIL-SAFE STRAP HOLE PER 767 NDTM 51-00-16 / 51-00-19.(<P>STR
- [SDR N6W2026F00003](https://openairdocs.org/sdr/N6W2026F00003.md): Retainer · bent · Oct 9, 2026 · N528GJ · Cndair CL6002C11
  > LOWER RETAINER SEAL BENT ON PAX DOOR BTW BS 311.75 - 8347.25. R & R LOWER RETAINER SEAL ON PAX DOOR IAW SRM 51-42-06.
- [SDR UIEA2026072000632](https://openairdocs.org/sdr/UIEA2026072000632.md): Rivet · sheared · Oct 9, 2026 · N419MC · Boeing 74748EF
  > QTY 01 DENT MARK AND QTY 01 SHEARED RIVET FOUND ON FUSELAGE SKIN FWD OF STA 2598, S26-38R, JACK PAD AREA. SHEARED RIVET ON FUSELAGE SKIN ON FWD OF STA 2598 BETWEEN S-26R AND S-38R EVALUATED AND FOUND STRUCTURALLY ACCEPTABLE TO LEAVE THE DENT AS-IS ALONG WITH
- [SDR UIEA2026072200636](https://openairdocs.org/sdr/UIEA2026072200636.md): Beam · damaged · Oct 9, 2026 · N419MC · Boeing 74748EF
  > WHILE ACCOMPLISHING SB747-53A2562 R3, FOUND EXISTING PANEL HOLE TOO CLOSE TO NEW BEAM (05EA) AT STA 340. FASTENER INTERFERENCE CONDITIONS WITH HORIZONTAL STIFFENERS ON LHS NOSE WHEEL WELL AT STA 340, WL 130 - WL 170 RECTIFIED WITH THE HORIZONTAL STIFFENER FLA
- [SDR UIEA2026072300639](https://openairdocs.org/sdr/UIEA2026072300639.md): Tension Tie · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > DURING HFEC OPEN HOLE INSPECTION ON LHS STA 920 TENSION TIE AND FRAME, FOUND 01EA FASTENER HOLE ON AFT CHANNEL WITH CRACK. CRACKED TENSION TIE AFT CHANNEL ON LHS STA 920 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW SRM 53-20-30-2R-1, REPAIR 1, FIGURE 201, BS
- [SDR UIEA2026081100742](https://openairdocs.org/sdr/UIEA2026081100742.md): Panel · damaged · Oct 9, 2026 · N419MC · Boeing 74748EF
  > WHILE ACCOMPLISHING SB747-53A2562 R3 AT STA 340, FOUND R/H PANEL FASTENER HOLES TOO CLOSE TO NEW BEAMS (02 EA) P/N: 141U1193-29 (WL130) AND P/N: 141U1193-27 (WL150)(<P>R/H PANEL NEW BEAMS (02 EA) P/N: 141U1193-29 (WL130) AND P/N: 141U1193-27 (WL150) REPAIRED A
- [SDR UIEA2026081200743](https://openairdocs.org/sdr/UIEA2026081200743.md): Tee Fitting · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > LOWER FUSELAGE: STA 250 TO STA 260 FWD BULKHEAD R/H SIDE T-CHORD FOUND CRACKED.(<P >AT R/H NOSE W/W FWD BULKHEAD STA 250 TO STA 260, CRACKED T-CHORD REMOVED AND INSTALLED WITH NEW FABRICATED T-CHORD AS PER EN 3565-26 REV.0. REPAIR CLASSIFIED AS "MAJOR" REPAIR
- [SDR UIEA2026081900781](https://openairdocs.org/sdr/UIEA2026081900781.md): Tee Fitting · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > LOWER FUSELAGE, BS 250 - 260, FWD BULKHEAD LT SIDE TEE FITTING FOUND CRACKED. A NEW TEE FITTING FABRICATED IAW EN 3564-26 REV. 0. R & R IAW SRM 51-40-02-0G-0, REV 107.
- [SDR UIEA2026082400792](https://openairdocs.org/sdr/UIEA2026082400792.md): Doubler · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > SUSPECTED CRACK ON MED L1 DOOR UPPER HINGE CUTOUT DOUBLER EDGE. DOUBLER FOR MED L1 DOOR UPPER HINGE CUTOUT, REMOVED AND A NEW DOUBLER FABRICATED & INSTALLED IAW EN 3413-26, REV 0.
- [SDR UIEA2026091700881](https://openairdocs.org/sdr/UIEA2026091700881.md): Door Frame · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > MAIN DECK L5 DOOR CUTOUT AREA AT BS 2220, STRINGER 18L FOUND CRACKED. L5 DOOR CUTOUT AREA REPAIRED IAW EN 3574-26, REV 0, & SRM 53-00-03-2R-1, REPAIR 1, REV 107.
- [SDR UIEA2026092000887](https://openairdocs.org/sdr/UIEA2026092000887.md): Door Frame · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > DURING HFEC INSPECTION ON DOOR STOP SUPPORT FITTINGS AT S16L, BS 2231, FOUND ONE LOWEST FWD HOLE WITH A CRACK INDICATION AT STRAP SIDE 3 & 9 O'CLOCK POSITION LOOKING OTBD. CRACK ON BS 2231 S16L. FRAME STRAP TRIMMED OUT & REPAIR CARRIED OUT IAW EN 3430-26, RE
- [SDR UIEA2026093000933](https://openairdocs.org/sdr/UIEA2026093000933.md): Door Sill · corroded · Oct 9, 2026 · N419MC · Boeing 74748EF
  > AFT CARGO DOOR LOWER SILL FOUND CORRODED. CORRODED DOOR SILL ON AFT CARGO DOOR AREA REMOVED AND REPLACED, AND REPAIR CARRIED OUT AS PER SRM 51-40-2-0G-0 REV. 107 AND EN 3557-26, REV. 0. REPAIR CLASSIFIED AS "MAJOR" AND CATEGORIZED AS "CATEGORY A" PERMANENT RE
- [SDR UIEA2026100300940](https://openairdocs.org/sdr/UIEA2026100300940.md): Door Frame · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > DURING HFEC INSPECTION ON LOWER LOBE AFT CARGO DOOR CUTOUT FORWARD UPPER CORNERS, FOUND CRACK APPROX 0.3" IN LENGTH AS MARKED(<P>DOUBLER REPAIR CARRIED OUT ON THE LOWER LOBE AFT CARGO DOOR CUTOUT FWD UPPER CORNER CRACKED AREA AS PER SRM 53-60-01-2R-3 REPAIR 3,
- [SDR UIEA2026100600965](https://openairdocs.org/sdr/UIEA2026100600965.md): Tension Tie · cracked · Oct 9, 2026 · N419MC · Boeing 74748EF
  > DURING HFEC OPEN HOLE INSPECTION ON LHS STA 920 TENSION TIE AND FRAME, FOUND 01 EA FASTENER HOLE ON AFT CHANNEL WITH CRACK. TENSION TIE AFT CHANNEL TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW SRM 53-20-30-2R-1, REPAIR 1, FIGURE 201, REV. 107. REPAIR CLASSIF
- [SDR UIEA2026100700966](https://openairdocs.org/sdr/UIEA2026100700966.md): Support Frame · damaged · Oct 9, 2026 · N419MC · Boeing 74748EF
  > HFEC OPEN HOLE INSPECTION CARRIED OUT ON 02 EA FASTENER HOLES AT STA 2598 BLKHD FRAME SUPPORT STA 2598 BELOW S-11L AND FOUND 02 EA HOLES DAMAGED ON THE 2ND LAYER, VIEW I/B AND FITTING HOLES. DAMAGED AREAS ON BS 2598 BULKHEAD FRAME SUPPORT AREAS REPAIRED IAW E
- [SDR FDEA202610091500](https://openairdocs.org/sdr/FDEA202610091500.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F
  > CENTER W/W - CENTER W/W FORWARD BULKHEAD LEFT HAND T - FITTING UPPER CORNER SUSPECT CRACK AT STATION 1368.650
- [SDR FDEA202610091499](https://openairdocs.org/sdr/FDEA202610091499.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F
  > CENTER W/W - CENTER W/W FORWARD BULKHEAD RIGHT HAND T - FITTING UPPER CORNER SUSPECT CRACK AT STATION 1368.650.
- [SDR FDEA202610091498](https://openairdocs.org/sdr/FDEA202610091498.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F
  > PER E.A.#1-5310-T0378549 REVISION.A PART 3 TITLE: FUSELAGE-MAINFRAME-CRACK REPAIR ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 595, REQUIRES REPLACEMENT OF FITTING OR CONTACT FEDEX ES FOR PERMANENT REPAIR PLAN.(FITTING ASSEMBLY PART NUMBER: A
- [SDR MASA20261022235](https://openairdocs.org/sdr/MASA20261022235.md): Seal Rest · corroded · Oct 8, 2026 · N83329 · Emb ERJ170200LR
  > DURING HEAVY CHECK, INSPECTIONS ON FWD CARGO CUTOUT, CORRODED LOWER AFT SEAL REST FR 25 R/H, STR 25 R/H REMOVED AND REPLACED IAW ERJ 175 AMM 20-10-01. NRC # 4502703-1000-0025, REV 103 DATED APR-25-2025.
- [SDR MASA20261022234](https://openairdocs.org/sdr/MASA20261022234.md): Seal Rest · corroded · Oct 8, 2026 · N83329 · Emb ERJ170200LR
  > DURING HEAVY CHECK, INSPECTIONS OF FWD CARGO, CORRODED LOWER FWD CORNER SEAL REST, FR 24 R/H, STR 25 R/H.REMOVED AND REPLACED WITH NEW IAW ERJ 175 AMM 20-10-01, NRC# 4502703-1000-0024. REV 103 DATED APR-25-2025.

Next page: https://openairdocs.org/jasc/5310/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 jasc_code = '5310'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5310/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.