# Service difficulty reports: N930UP, cancelled Nov 21, 2007

A list on [N930UP, cancelled Nov 21, 2007](https://openairdocs.org/deregistered/N930UP-2007-11-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 175 reports

- [SDR UPS06248609](https://openairdocs.org/sdr/UPS06248609.md): Battery · discharged · Nov 12, 2006 · N930UP · Boeing 72722C · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM 35-50-67. OPS CHECK GOOD.
- [SDR UPS06246477](https://openairdocs.org/sdr/UPS06246477.md): Door · damaged · Mar 21, 2006 · N930UP · Boeing 72722C · Air Conditioning Doors
  > FOUND LT AC PACK DOOR CAME OFF IN FLIGHT AND DAMAGING FUSELAGE AFT OF PACK. RT DOOR IS HANGING BY AFT HINGE AND IS BEYOND REPAIR.
- [SDR UPS06246446](https://openairdocs.org/sdr/UPS06246446.md): Wire · loose · Mar 15, 2006 · N930UP · Boeing 72722C · Light System Wiring
  > EMERGENCY EXIT LIGHTS INOP. FOUND BOTTOM C/B PANEL LIGHTING INOP ON LEFT SIDE OF COCKPIT. FOUND POWER WIRE LOOSE. TIGHTENED LOOSE POWER WIRE. OPS CK GOOD.
- [SDR UPS06246517](https://openairdocs.org/sdr/UPS06246517.md): Battery · inoperative · Mar 14, 2006 · N930UP · Boeing 72722C · Emergency Lighting
  > ON PREDEPARTURE CK, FOUND EMERGENCY EXIT LIGHT SWITCH IN ON POSITION. REMOVED AND REPLACED BATTERIES IAW MM 33-50-11-2. OPS CKS NORMAL.
- [SDR UPS06246393](https://openairdocs.org/sdr/UPS06246393.md): Skin · dented · Feb 28, 2006 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SP REF DMI D-320435, DENT AT FS 1163 AT STR 20R INCOMING MEASUREMENT (APPROX) OF 3.0"DIA X.200 DEEP AND GOUGED 2.0" X.005"DEEP. CUT OUT DAMAGE AT FS 1163, STR 20R IAW SRM 53-30-03 FIG 5. FABRICATED AND INSTALLED REPAIR FILLERS (2EA), AND RE
- [SDR UPS05245314](https://openairdocs.org/sdr/UPS05245314.md): Skin · cracked · Aug 30, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > SUSPECT SKIN CRACK AT BS 364 STR 3 LT. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 53030-3 FIG 3A.
- [SDR UPS05245313](https://openairdocs.org/sdr/UPS05245313.md): Clip · cracked · Aug 29, 2005 · N930UP · Boeing 72722C · Aerodynamic Fairings
  > RT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.
- [SDR UPS05245312](https://openairdocs.org/sdr/UPS05245312.md): Frame · corroded · Aug 29, 2005 · N930UP · Boeing 72722C · Aerodynamic Fairings
  > BODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7.
- [SDR UPS05245357](https://openairdocs.org/sdr/UPS05245357.md): Skin · cracked · Aug 25, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > SUSPECT SKIN CRACK AT UPPER FWD ENTRY DOOR CUT OUT BETWEEN STR 5 AND 6 L. PLEASE CARRY OUT NDI AND RECIFITY. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5330-1460-D OPT 1.
- [SDR UPS05245372](https://openairdocs.org/sdr/UPS05245372.md): Web · cracked · Aug 23, 2005 · N930UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, NLG W/W CEILING AT BS 290 LBL 0 HAS SUSPECT CRACKS AT FASTENER HEADS. WEB REPLACED IAW SRM 51-20-1 AND DWG 65-18416.
- [SDR UPS05245356](https://openairdocs.org/sdr/UPS05245356.md): Door · corroded · Aug 23, 2005 · N930UP · Boeing 72722C · Landing Gear Doors
  > NLG FWD LT DOOR HAS CORROSION UNDER SEAL AT I/B END. CORRODED SECTION REPLACED WITH FABRICATED SECTION IAW SRM 51-20-1 AND DWG 65-17563.
- [SDR UPS05245317](https://openairdocs.org/sdr/UPS05245317.md): Stringer · corroded · Aug 22, 2005 · N930UP · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > AREA OF SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE AT BS 295 STR22R. CORROSION FOUND TO BE ON STRINGER 22R BETWEEN BS 204-316. STRINGER SECTION REPLACED BETWEEN BS 304 AND 320 IAW SRM 53-10-3 FIG 1.
- [SDR UPS05245316](https://openairdocs.org/sdr/UPS05245316.md): Skin · scratched · Aug 22, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > LIGHT SURFACE SCRATCHES FOUND ON SKIN AT BS 1263 BETWEEN S5L AND 6L. DAMAGED AREA FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13.
- [SDR UPS04243231](https://openairdocs.org/sdr/UPS04243231.md): Panel · delaminated · Sep 29, 2004 · N930UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER PER MM 27-62-01. OPS CHECK NORMAL.
- [SDR UPS04242321](https://openairdocs.org/sdr/UPS04242321.md): Support · cracked · Apr 27, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02.
- [SDR UPS04242344](https://openairdocs.org/sdr/UPS04242344.md): Frame · cracked · Apr 26, 2004 · N930UP · Boeing 72722C · Vertical Stabilizer
  > INSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02
- [SDR UPS04242316](https://openairdocs.org/sdr/UPS04242316.md): Pulley Bracket · cracked · Apr 26, 2004 · N930UP · Boeing 72722C · Rudder Control System
  > INSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED.
- [SDR UPS04242343](https://openairdocs.org/sdr/UPS04242343.md): Skin · cracked · Apr 24, 2004 · N930UP · Boeing 72722C · Engine Thrust Reverser
  > INSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CARRIED OUT AROUND STO
- [SDR UPS04242341](https://openairdocs.org/sdr/UPS04242341.md): Skin · chafed · Apr 16, 2004 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. REPAIR CARRIED OUT IAW
- [SDR UPS04242358](https://openairdocs.org/sdr/UPS04242358.md): Rib · cracked · Apr 15, 2004 · N930UP · Boeing 72722C · Service Doors
  > INSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02
- [SDR UPS04242356](https://openairdocs.org/sdr/UPS04242356.md): Retainer · corroded · Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01
- [SDR UPS04242342](https://openairdocs.org/sdr/UPS04242342.md): Cargo Track · corroded · Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2
- [SDR UPS04242355](https://openairdocs.org/sdr/UPS04242355.md): Retainer · corroded · Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01
- [SDR UPS04242320](https://openairdocs.org/sdr/UPS04242320.md): Pressure Panel · cracked · Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, INSTALLED FABRICATED
- [SDR UPS04242318](https://openairdocs.org/sdr/UPS04242318.md): Doubler · corroded · Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10-02 AND 51-30-02.
- [SDR UPS04242357](https://openairdocs.org/sdr/UPS04242357.md): Web · cracked · Apr 13, 2004 · N930UP · Boeing 72722C · Leading Edge Devices
  > INSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02
- [SDR UPS03240913](https://openairdocs.org/sdr/UPS03240913.md): Skin · cracked · Jun 26, 2003 · N930UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS.375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL AS PER SRM ADDENDUM EO B727-5330-5128A.
- [SDR UPS02239758](https://openairdocs.org/sdr/UPS02239758.md): Hinge · cracked · Oct 10, 2002 · N930UP · Boeing 72722C · Passenger/Crew Doors
  > UPPER HINGE ARM OF AFT ENTRY DOOR CRACKED. HINGE REPLACED. FUNCTION AND OPERATION CHECK CARRIED OUT IAW MM 52-13-02 AND 52-13-00.
- [SDR UPS02239609](https://openairdocs.org/sdr/UPS02239609.md): Shear Tie · cracked · Oct 4, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C+SI STR.SHEAR TIE CRACKED AT STR.5 R/H BS1050. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW 51-20-1+51-40-3
- [SDR UPS02239769](https://openairdocs.org/sdr/UPS02239769.md): Spar · corroded · Oct 3, 2002 · N930UP · Boeing 72722C · Wing Spar
  > DURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND STIFFENERS FABRICATED IAW DRG NR 65C21531 REPAIR COMPLETED IAW SMRO EO 2002-052-013. UPS ENG FILE NR
- [SDR UPS02239767](https://openairdocs.org/sdr/UPS02239767.md): Beam · corroded · Sep 30, 2002 · N930UP · Boeing 72722C · Wing, Landing Gear Attach Fittings
  > DURING REMOVAL OF T/E PANEL ATTACHED TO LOWER SURFACE OF RT MLG SUPPORT BEAM, CORROSION NOTED AROUND MLG SUPPORT BEAM FASTENER HOLE. CORROSION REMOVED AROUND HOLE IAW SRM 51-10-06. HFEC C/O ON FASTENER HOLE AND COUNTER BORE IN THE ABOVE AREA IAW B727 N DTM P
- [SDR UPS02239741](https://openairdocs.org/sdr/UPS02239741.md): Frame · damaged · Sep 30, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI DURING REPAIR OF FRAME BS 560 STR. 7R DAMAGE WAS FOUND ON EXISTING R EPAIR ABOVE AT S5R - 6R REPAIR TO FRAME CARRIED OUT IAW SRM 53-10-4 FIG 2
- [SDR UPS02239740](https://openairdocs.org/sdr/UPS02239740.md): Pressure Panel · damaged · Sep 30, 2002 · N930UP · Boeing 72722C · Fuselage Main, Bulkhead
  > PRESS WEB AT BS 740 BULKHEAD DAMAGED AT LWR END WHERE IT ATTACHS TO 740 RT FITTING. DAMAGE BLENDED OUT AND REPAIRED PER SRM 53-10-9 FIG 4.
- [SDR UPS02239774](https://openairdocs.org/sdr/UPS02239774.md): Riser · corroded · Sep 24, 2002 · N930UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C+SI CORROSION ON RISER #5 FOUND TO BE OUTSIDE LIMITS- REF NRC 480122.(AI RSTAIR DOOR) RISER REPLACED IAW SRM ADDENDIUM EO B727-5260-1551-A.
- [SDR UPS02239773](https://openairdocs.org/sdr/UPS02239773.md): Hinge Pin · corroded · Sep 24, 2002 · N930UP · Boeing 72722C · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-10-01 STEPS 3 AND 4.
- [SDR UPS02239719](https://openairdocs.org/sdr/UPS02239719.md): Riser · corroded · Sep 24, 2002 · N930UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C&SI CORROSION ON RISER #6 ON AFT AIRSTAIRS FOUND TO BE OUTSIDE LIMITS RE F. NRC 480122 #6 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A
- [SDR UPS02239718](https://openairdocs.org/sdr/UPS02239718.md): Riser · corroded · Sep 24, 2002 · N930UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C&SI CORROSION ON RISER #8 ON AFT AIRSTAIRS DOOR FOUND TO BE OUTSIDE LIMI TS REF. NRC 480122 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A
- [SDR UPS02239716](https://openairdocs.org/sdr/UPS02239716.md): Panel · cracked · Sep 24, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL PANEL RH SIDE ALONG ROW OF FASTNERS BELOW FW D RH PRESSURE PANEL BS 239 FASTENERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-2. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2 & SRM 51-30-2
- [SDR UPS02239715](https://openairdocs.org/sdr/UPS02239715.md): Panel · cracked · Sep 24, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL SIDE PANEL RH SIDE ALONG ROW OF FASTENERS AF T OF FWD RH PANEL BS 250 FASTNERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-02. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2
- [SDR UPS02239557](https://openairdocs.org/sdr/UPS02239557.md): Pin · corroded · Sep 24, 2002 · N930UP · Boeing 72722C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS HORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM 55-10-01
- [SDR UPS02239768](https://openairdocs.org/sdr/UPS02239768.md): Keelbeam · cracked · Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, Keel
  > CRACKS RT KEEL BEAM VERTICAL WEB FWD OF APU CUT OUT. REPAIR IAW EO B727-5330-1995-B.
- [SDR UPS02239717](https://openairdocs.org/sdr/UPS02239717.md): Frame · corroded · Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, Frame
  > BS 740 BULKHEAD LWR CHORD FOUND CORRODED DURING REMOVAL TO FACILITATE FITTING REPLACEMENT. SECTION OF CHORD REPLACED IAW DRAWING 65C13724.
- [SDR UPS02239558](https://openairdocs.org/sdr/UPS02239558.md): Intercostal · cracked · Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 294 & 284 LBL 5 REMOVED INTERCOSTAL IAW SRM 51-30-2 FABRICATED INTERCOSTAL IAW SRM 53-10-2 & SRM 51-20-4 INSTALLED INTERCOSTAL IAW SRM 51-30-2
- [SDR UPS02239607](https://openairdocs.org/sdr/UPS02239607.md): Rib · cracked · Sep 22, 2002 · N930UP · Boeing 72722C · Wing Main, Frame Structure
  > INSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12.
- [SDR UPS02239714](https://openairdocs.org/sdr/UPS02239714.md): Seat Track · corroded · Sep 20, 2002 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND NUT BS 380 LBL 45.5 ON SEAT TRACK. REMOVED DAMAGED SECTION IAW SRM 51-30-2, REPAIRED IAW SRM 53-10-5.
- [SDR UPS02239639](https://openairdocs.org/sdr/UPS02239639.md): Frame · dented · Sep 20, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C+SI DENT IN FRAME BS 560 STR7 R/H REPAIRED IAW SRM 53-10-4 FIG 1
- [SDR UPS02239766](https://openairdocs.org/sdr/UPS02239766.md): Support Fitting · corroded · Sep 19, 2002 · N930UP · Boeing 72722C · Main Landing Gear
  > INSPECTION TYPE:C+SI CORROSION ON INNER FACE OF RH MLG TRUNNION SUPPORT FITTING. RH MLG TRUNNION SUPPORT FITTING REPLACED.
- [SDR UPS02239756](https://openairdocs.org/sdr/UPS02239756.md): Stiffener · corroded · Sep 19, 2002 · N930UP · Boeing 72722C · Wing, Center Box
  > BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.
- [SDR UPS02239745](https://openairdocs.org/sdr/UPS02239745.md): Frame · cracked · Sep 19, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI CRACK ON LWR AFT FLANGE OF FRAME BS 930 R/H AT MLG PRESS. WEB REPAIRS TO S15 & S16 CARRIED OUT IAW SRM 53-10-3. FRAME REPAIR BS 9 20 SPLICE FABRICATED IAW SRM 51-10-3 NEW 930 FITTING INSTALLED IAW D RG 65-16336 &65-18383 SRM 51-30-3 &
- [SDR UPS02239721](https://openairdocs.org/sdr/UPS02239721.md): Frame · cracked · Sep 19, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI LWR AFT CARGO BAY, FRAME (BS1030)TO FUSELAGE SKIN ATTACH POINT IS CR ACKED IN BEND RADIUS BETWEEN STR 25 AND STR. 26L/H FRAME REPAIRED IAW SRM 53-10-4 FIG 11

Next page: https://openairdocs.org/deregistered/N930UP-2007-11-21/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 n_number = 'N930UP' AND deregistration_id = 'N930UP-2007-11-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N930UP-2007-11-21/reports

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